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Ardupilot2/Tools/autotest/arduplane.py
Paul Riseborough 2b027a7265 Tools: re-work copter and plane loss of GPS auto tests 
Explicitly test time taken to reset to GPS loss and regain of lock for copter without and plane with dead reckoning assistance.
2024-06-09 14:25:02 +10:00

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'''
Fly ArduPlane in SITL
AP_FLAKE8_CLEAN
'''
from __future__ import print_function
import math
import os
import signal
import time
from pymavlink import quaternion
from pymavlink import mavutil
from pymavlink.rotmat import Vector3
import vehicle_test_suite
from vehicle_test_suite import AutoTestTimeoutException
from vehicle_test_suite import NotAchievedException
from vehicle_test_suite import OldpymavlinkException
from vehicle_test_suite import PreconditionFailedException
from vehicle_test_suite import Test
from vehicle_test_suite import WaitModeTimeout
from pysim import vehicleinfo
from pysim import util
import operator
# get location of scripts
testdir = os.path.dirname(os.path.realpath(__file__))
SITL_START_LOCATION = mavutil.location(-35.362938, 149.165085, 585, 354)
WIND = "0,180,0.2" # speed,direction,variance
class AutoTestPlane(vehicle_test_suite.TestSuite):
@staticmethod
def get_not_armable_mode_list():
return []
@staticmethod
def get_not_disarmed_settable_modes_list():
return ["FOLLOW"]
@staticmethod
def get_no_position_not_settable_modes_list():
return []
@staticmethod
def get_position_armable_modes_list():
return ["GUIDED", "AUTO"]
@staticmethod
def get_normal_armable_modes_list():
return ["MANUAL", "STABILIZE", "ACRO"]
def log_name(self):
return "ArduPlane"
def default_speedup(self):
return 100
def test_filepath(self):
return os.path.realpath(__file__)
def sitl_start_location(self):
return SITL_START_LOCATION
def defaults_filepath(self):
return os.path.join(testdir, 'default_params/plane-jsbsim.parm')
def set_current_test_name(self, name):
self.current_test_name_directory = "ArduPlane_Tests/" + name + "/"
def default_frame(self):
return "plane-elevrev"
def apply_defaultfile_parameters(self):
# plane passes in a defaults_filepath in place of applying
# parameters afterwards.
pass
def is_plane(self):
return True
def get_stick_arming_channel(self):
return int(self.get_parameter("RCMAP_YAW"))
def get_disarm_delay(self):
return int(self.get_parameter("LAND_DISARMDELAY"))
def set_autodisarm_delay(self, delay):
self.set_parameter("LAND_DISARMDELAY", delay)
def takeoff(self, alt=150, alt_max=None, relative=True, mode=None, timeout=None):
"""Takeoff to altitude."""
if mode == "TAKEOFF":
return self.takeoff_in_TAKEOFF(alt=alt, relative=relative, timeout=timeout)
return self.takeoff_in_FBWA(alt=alt, alt_max=alt_max, relative=relative, timeout=timeout)
def takeoff_in_TAKEOFF(self, alt=150, relative=True, mode=None, alt_epsilon=2, timeout=None):
if relative is not True:
raise ValueError("Only relative alt supported ATM")
self.change_mode("TAKEOFF")
self.context_push()
self.set_parameter('TKOFF_ALT', alt)
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_altitude(alt-alt_epsilon, alt+alt_epsilon, relative=True, timeout=timeout)
self.context_pop()
def takeoff_in_FBWA(self, alt=150, alt_max=None, relative=True, mode=None, timeout=30):
if alt_max is None:
alt_max = alt + 30
self.change_mode("FBWA")
self.wait_ready_to_arm()
self.arm_vehicle()
# some rudder to counteract the prop torque
self.set_rc(4, 1700)
# some up elevator to keep the tail down
self.set_rc(2, 1200)
# get it moving a bit first
self.set_rc(3, 1300)
self.wait_groundspeed(6, 100)
# a bit faster again, straighten rudder
self.set_rc_from_map({
3: 1600,
4: 1500,
})
self.wait_groundspeed(12, 100)
# hit the gas harder now, and give it some more elevator
self.set_rc_from_map({
2: 1100,
3: 2000,
})
# gain a bit of altitude
self.wait_altitude(alt, alt_max, timeout=timeout, relative=relative)
# level off
self.set_rc(2, 1500)
self.progress("TAKEOFF COMPLETE")
def fly_left_circuit(self):
"""Fly a left circuit, 200m on a side."""
self.change_mode('FBWA')
self.set_rc(3, 2000)
self.wait_level_flight()
self.progress("Flying left circuit")
# do 4 turns
for i in range(0, 4):
# hard left
self.progress("Starting turn %u" % i)
self.set_rc(1, 1000)
self.wait_heading(270 - (90*i), accuracy=10)
self.set_rc(1, 1500)
self.progress("Starting leg %u" % i)
self.wait_distance(100, accuracy=20)
self.progress("Circuit complete")
def fly_RTL(self):
"""Fly to home."""
self.progress("Flying home in RTL")
target_loc = self.homeloc
target_loc.alt += 100
self.change_mode('RTL')
self.wait_location(target_loc,
accuracy=120,
height_accuracy=20,
timeout=180)
self.progress("RTL Complete")
def NeedEKFToArm(self):
"""Ensure the EKF must be healthy for the vehicle to arm."""
self.progress("Ensuring we need EKF to be healthy to arm")
self.set_parameter("SIM_GPS_DISABLE", 1)
self.context_collect("STATUSTEXT")
tstart = self.get_sim_time()
success = False
for run_cmd in self.run_cmd, self.run_cmd_int:
while not success:
if self.get_sim_time_cached() - tstart > 60:
raise NotAchievedException("Did not get correct failure reason")
run_cmd(mavutil.mavlink.MAV_CMD_RUN_PREARM_CHECKS)
try:
self.wait_statustext(".*AHRS: not using configured AHRS type.*", timeout=1, check_context=True, regex=True)
success = True
continue
except AutoTestTimeoutException:
pass
self.set_parameter("SIM_GPS_DISABLE", 0)
self.wait_ready_to_arm()
def fly_LOITER(self, num_circles=4):
"""Loiter where we are."""
self.progress("Testing LOITER for %u turns" % num_circles)
self.change_mode('LOITER')
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
initial_alt = m.alt
self.progress("Initial altitude %u\n" % initial_alt)
while num_circles > 0:
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
num_circles -= 1
self.progress("Loiter %u circles left" % num_circles)
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
final_alt = m.alt
self.progress("Final altitude %u initial %u\n" %
(final_alt, initial_alt))
self.change_mode('FBWA')
if abs(final_alt - initial_alt) > 20:
raise NotAchievedException("Failed to maintain altitude")
self.progress("Completed Loiter OK")
def fly_CIRCLE(self, num_circles=1):
"""Circle where we are."""
self.progress("Testing CIRCLE for %u turns" % num_circles)
self.change_mode('CIRCLE')
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
initial_alt = m.alt
self.progress("Initial altitude %u\n" % initial_alt)
while num_circles > 0:
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
num_circles -= 1
self.progress("CIRCLE %u circles left" % num_circles)
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
final_alt = m.alt
self.progress("Final altitude %u initial %u\n" %
(final_alt, initial_alt))
self.change_mode('FBWA')
if abs(final_alt - initial_alt) > 20:
raise NotAchievedException("Failed to maintain altitude")
self.progress("Completed CIRCLE OK")
def wait_level_flight(self, accuracy=5, timeout=30):
"""Wait for level flight."""
tstart = self.get_sim_time()
self.progress("Waiting for level flight")
self.set_rc(1, 1500)
self.set_rc(2, 1500)
self.set_rc(4, 1500)
while self.get_sim_time_cached() < tstart + timeout:
m = self.mav.recv_match(type='ATTITUDE', blocking=True)
roll = math.degrees(m.roll)
pitch = math.degrees(m.pitch)
self.progress("Roll=%.1f Pitch=%.1f" % (roll, pitch))
if math.fabs(roll) <= accuracy and math.fabs(pitch) <= accuracy:
self.progress("Attained level flight")
return
raise NotAchievedException("Failed to attain level flight")
def change_altitude(self, altitude, accuracy=30):
"""Get to a given altitude."""
self.change_mode('FBWA')
alt_error = self.mav.messages['VFR_HUD'].alt - altitude
if alt_error > 0:
self.set_rc(2, 2000)
else:
self.set_rc(2, 1000)
self.wait_altitude(altitude-accuracy/2, altitude+accuracy/2)
self.set_rc(2, 1500)
self.progress("Reached target altitude at %u" %
self.mav.messages['VFR_HUD'].alt)
return self.wait_level_flight()
def axial_left_roll(self, count=1):
"""Fly a left axial roll."""
# full throttle!
self.set_rc(3, 2000)
self.change_altitude(self.homeloc.alt+300)
# fly the roll in manual
self.change_mode('MANUAL')
while count > 0:
self.progress("Starting roll")
self.set_rc(1, 1000)
try:
self.wait_roll(-150, accuracy=90)
self.wait_roll(150, accuracy=90)
self.wait_roll(0, accuracy=90)
except Exception as e:
self.set_rc(1, 1500)
raise e
count -= 1
# back to FBWA
self.set_rc(1, 1500)
self.change_mode('FBWA')
self.set_rc(3, 1700)
return self.wait_level_flight()
def inside_loop(self, count=1):
"""Fly a inside loop."""
# full throttle!
self.set_rc(3, 2000)
self.change_altitude(self.homeloc.alt+300)
# fly the loop in manual
self.change_mode('MANUAL')
while count > 0:
self.progress("Starting loop")
self.set_rc(2, 1000)
self.wait_pitch(-60, accuracy=20)
self.wait_pitch(0, accuracy=20)
count -= 1
# back to FBWA
self.set_rc(2, 1500)
self.change_mode('FBWA')
self.set_rc(3, 1700)
return self.wait_level_flight()
def set_attitude_target(self, tolerance=10):
"""Test setting of attitude target in guided mode."""
self.change_mode("GUIDED")
steps = [{"name": "roll-over", "roll": 60, "pitch": 0, "yaw": 0, "throttle": 0, "type_mask": 0b10000001},
{"name": "roll-back", "roll": 0, "pitch": 0, "yaw": 0, "throttle": 0, "type_mask": 0b10000001},
{"name": "pitch-up+throttle", "roll": 0, "pitch": 20, "yaw": 0, "throttle": 1, "type_mask": 0b11000010},
{"name": "pitch-back", "roll": 0, "pitch": 0, "yaw": 0, "throttle": 0, "type_mask": 0b10000010}]
state_wait = "wait"
state_hold = "hold"
try:
for step in steps:
step_start = self.get_sim_time_cached()
state = state_wait
state_start = self.get_sim_time_cached()
while True:
m = self.mav.recv_match(type='ATTITUDE',
blocking=True,
timeout=0.1)
now = self.get_sim_time_cached()
if now - step_start > 30:
raise AutoTestTimeoutException("Manuevers not completed")
if m is None:
continue
angle_error = 0
if (step["type_mask"] & 0b00000001) or (step["type_mask"] == 0b10000000):
angle_error += abs(math.degrees(m.roll) - step["roll"])
if (step["type_mask"] & 0b00000010) or (step["type_mask"] == 0b10000000):
angle_error += abs(math.degrees(m.pitch) - step["pitch"])
if (step["type_mask"] & 0b00000100) or (step["type_mask"] == 0b10000000):
# Strictly we should angle wrap, by plane doesn't support yaw correctly anyway so its not tested here
angle_error += abs(math.degrees(m.yaw) - step["yaw"])
# Note were not checking throttle, however the SITL plane needs full throttle to meet the
# target pitch attitude, Pitch test will fail without throttle override
if state == state_wait:
# Reduced tolerance for initial trigger
if angle_error < (tolerance * 0.25):
state = state_hold
state_start = now
# Allow 10 seconds to reach attitude
if (now - state_start) > 10:
raise NotAchievedException(step["name"] + ": Failed to get to set attitude")
elif state == state_hold:
# Give 2 seconds to stabilize
if (now - state_start) > 2 and not (angle_error < tolerance):
raise NotAchievedException(step["name"] + ": Failed to hold set attitude")
# Hold for 10 seconds
if (now - state_start) > 12:
# move onto next step
self.progress("%s Done" % (step["name"]))
break
self.progress("%s %s error: %f" % (step["name"], state, angle_error))
time_boot_millis = 0 # FIXME
target_system = 1 # FIXME
target_component = 1 # FIXME
type_mask = step["type_mask"] ^ 0xFF # FIXME
# attitude in radians:
q = quaternion.Quaternion([math.radians(step["roll"]),
math.radians(step["pitch"]),
math.radians(step["yaw"])])
self.mav.mav.set_attitude_target_send(time_boot_millis,
target_system,
target_component,
type_mask,
q,
0, # roll rate, not used in AP
0, # pitch rate, not used in AP
0, # yaw rate, not used in AP
step["throttle"])
except Exception as e:
self.change_mode('FBWA')
self.set_rc(3, 1700)
raise e
# back to FBWA
self.change_mode('FBWA')
self.set_rc(3, 1700)
self.wait_level_flight()
def test_stabilize(self, count=1):
"""Fly stabilize mode."""
# full throttle!
self.set_rc(3, 2000)
self.set_rc(2, 1300)
self.change_altitude(self.homeloc.alt+300)
self.set_rc(2, 1500)
self.change_mode('STABILIZE')
while count > 0:
self.progress("Starting roll")
self.set_rc(1, 2000)
self.wait_roll(-150, accuracy=90)
self.wait_roll(150, accuracy=90)
self.wait_roll(0, accuracy=90)
count -= 1
self.set_rc(1, 1500)
self.wait_roll(0, accuracy=5)
# back to FBWA
self.change_mode('FBWA')
self.set_rc(3, 1700)
return self.wait_level_flight()
def test_acro(self, count=1):
"""Fly ACRO mode."""
# full throttle!
self.set_rc(3, 2000)
self.set_rc(2, 1300)
self.change_altitude(self.homeloc.alt+300)
self.set_rc(2, 1500)
self.change_mode('ACRO')
while count > 0:
self.progress("Starting roll")
self.set_rc(1, 1000)
self.wait_roll(-150, accuracy=90)
self.wait_roll(150, accuracy=90)
self.wait_roll(0, accuracy=90)
count -= 1
self.set_rc(1, 1500)
# back to FBWA
self.change_mode('FBWA')
self.wait_level_flight()
self.change_mode('ACRO')
count = 2
while count > 0:
self.progress("Starting loop")
self.set_rc(2, 1000)
self.wait_pitch(-60, accuracy=20)
self.wait_pitch(0, accuracy=20)
count -= 1
self.set_rc(2, 1500)
# back to FBWA
self.change_mode('FBWA')
self.set_rc(3, 1700)
return self.wait_level_flight()
def test_FBWB(self, mode='FBWB'):
"""Fly FBWB or CRUISE mode."""
self.change_mode(mode)
self.set_rc(3, 1700)
self.set_rc(2, 1500)
# lock in the altitude by asking for an altitude change then releasing
self.set_rc(2, 1000)
self.wait_distance(50, accuracy=20)
self.set_rc(2, 1500)
self.wait_distance(50, accuracy=20)
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
initial_alt = m.alt
self.progress("Initial altitude %u\n" % initial_alt)
self.progress("Flying right circuit")
# do 4 turns
for i in range(0, 4):
# hard left
self.progress("Starting turn %u" % i)
self.set_rc(1, 1800)
try:
self.wait_heading(0 + (90*i), accuracy=20, timeout=60)
except Exception as e:
self.set_rc(1, 1500)
raise e
self.set_rc(1, 1500)
self.progress("Starting leg %u" % i)
self.wait_distance(100, accuracy=20)
self.progress("Circuit complete")
self.progress("Flying rudder left circuit")
# do 4 turns
for i in range(0, 4):
# hard left
self.progress("Starting turn %u" % i)
self.set_rc(4, 1900)
try:
self.wait_heading(360 - (90*i), accuracy=20, timeout=60)
except Exception as e:
self.set_rc(4, 1500)
raise e
self.set_rc(4, 1500)
self.progress("Starting leg %u" % i)
self.wait_distance(100, accuracy=20)
self.progress("Circuit complete")
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
final_alt = m.alt
self.progress("Final altitude %u initial %u\n" %
(final_alt, initial_alt))
# back to FBWA
self.change_mode('FBWA')
if abs(final_alt - initial_alt) > 20:
raise NotAchievedException("Failed to maintain altitude")
return self.wait_level_flight()
def fly_mission(self, filename, mission_timeout=60.0, strict=True, quadplane=False):
"""Fly a mission from a file."""
self.progress("Flying mission %s" % filename)
num_wp = self.load_mission(filename, strict=strict)-1
self.fly_mission_waypoints(num_wp, mission_timeout=mission_timeout, quadplane=quadplane)
def fly_mission_waypoints(self, num_wp, mission_timeout=60.0, quadplane=False):
self.set_current_waypoint(0, check_afterwards=False)
self.context_push()
self.context_collect('STATUSTEXT')
self.change_mode('AUTO')
self.wait_waypoint(1, num_wp, max_dist=60, timeout=mission_timeout)
self.wait_groundspeed(0, 0.5, timeout=mission_timeout)
if quadplane:
self.wait_statustext("Throttle disarmed", timeout=200, check_context=True)
else:
self.wait_statustext("Auto disarmed", timeout=60, check_context=True)
self.context_pop()
self.progress("Mission OK")
def DO_REPOSITION(self):
'''Test mavlink DO_REPOSITION command'''
self.progress("Takeoff")
self.takeoff(alt=50)
self.set_rc(3, 1500)
self.progress("Entering guided and flying somewhere constant")
self.change_mode("GUIDED")
loc = self.mav.location()
self.location_offset_ne(loc, 500, 500)
new_alt = 100
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
p5=int(loc.lat * 1e7),
p6=int(loc.lng * 1e7),
p7=new_alt, # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT,
)
self.wait_altitude(new_alt-10, new_alt, timeout=30, relative=True)
self.install_terrain_handlers_context()
self.location_offset_ne(loc, 500, 500)
terrain_height_wanted = 150
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
0,
0,
0,
0,
int(loc.lat*1e7),
int(loc.lng*1e7),
terrain_height_wanted, # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_TERRAIN_ALT,
)
# move to specific terrain-relative altitude and hold for <n> seconds
tstart = self.get_sim_time_cached()
achieve_start = None
tr = None
while True:
if self.get_sim_time_cached() - tstart > 120:
raise NotAchievedException("Did not move to correct terrain alt")
m = self.mav.recv_match(type='TERRAIN_REPORT',
blocking=True,
timeout=1)
tr = m
terrain_height_achieved = m.current_height
self.progress("terrain_alt=%f want=%f" %
(terrain_height_achieved, terrain_height_wanted))
if m is None:
continue
if abs(terrain_height_wanted - terrain_height_achieved) > 5:
if achieve_start is not None:
self.progress("Achieve stop")
achieve_start = None
elif achieve_start is None:
self.progress("Achieve start")
achieve_start = self.get_sim_time_cached()
if achieve_start is not None:
if self.get_sim_time_cached() - achieve_start > 10:
break
m = self.mav.recv_match(type='GLOBAL_POSITION_INT',
blocking=True,
timeout=1)
self.progress("TR: %s" % tr)
self.progress("GPI: %s" % m)
min_delta = 4
delta = abs(m.relative_alt/1000.0 - tr.current_height)
if abs(delta < min_delta):
raise NotAchievedException("Expected altitude delta (want=%f got=%f)" %
(min_delta, delta))
self.fly_home_land_and_disarm(timeout=180)
def ExternalPositionEstimate(self):
'''Test mavlink EXTERNAL_POSITION_ESTIMATE command'''
if not hasattr(mavutil.mavlink, 'MAV_CMD_EXTERNAL_POSITION_ESTIMATE'):
raise OldpymavlinkException("pymavlink too old; upgrade pymavlink to get MAV_CMD_EXTERNAL_POSITION_ESTIMATE") # noqa
self.change_mode("TAKEOFF")
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_altitude(48, 52, relative=True)
loc = self.mav.location()
self.location_offset_ne(loc, 2000, 2000)
# setting external position fail while we have GPS lock
self.progress("set new position with GPS")
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_EXTERNAL_POSITION_ESTIMATE,
p1=self.get_sim_time()-1, # transmit time
p2=0.5, # processing delay
p3=50, # accuracy
p5=int(loc.lat * 1e7),
p6=int(loc.lng * 1e7),
p7=float("NaN"), # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL,
want_result=mavutil.mavlink.MAV_RESULT_FAILED,
)
self.progress("disable the GPS")
self.run_auxfunc(
65,
2,
want_result=mavutil.mavlink.MAV_RESULT_ACCEPTED
)
# fly for a bit to get into non-aiding state
self.progress("waiting 20 seconds")
tstart = self.get_sim_time()
while self.get_sim_time() < tstart + 20:
self.wait_heartbeat()
self.progress("getting base position")
gpi = self.mav.recv_match(
type='GLOBAL_POSITION_INT',
blocking=True,
timeout=5
)
loc = mavutil.location(gpi.lat*1e-7, gpi.lon*1e-7, 0, 0)
self.progress("set new position with no GPS")
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_EXTERNAL_POSITION_ESTIMATE,
p1=self.get_sim_time()-1, # transmit time
p2=0.5, # processing delay
p3=50, # accuracy
p5=gpi.lat+1,
p6=gpi.lon+1,
p7=float("NaN"), # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL,
want_result=mavutil.mavlink.MAV_RESULT_ACCEPTED
)
self.progress("waiting 3 seconds")
tstart = self.get_sim_time()
while self.get_sim_time() < tstart + 3:
self.wait_heartbeat()
gpi2 = self.mav.recv_match(
type='GLOBAL_POSITION_INT',
blocking=True,
timeout=5
)
loc2 = mavutil.location(gpi2.lat*1e-7, gpi2.lon*1e-7, 0, 0)
dist = self.get_distance(loc, loc2)
self.progress("dist is %.1f" % dist)
if dist > 200:
raise NotAchievedException("Position error dist=%.1f" % dist)
self.progress("re-enable the GPS")
self.run_auxfunc(
65,
0,
want_result=mavutil.mavlink.MAV_RESULT_ACCEPTED
)
self.progress("flying home")
self.fly_home_land_and_disarm()
def DeepStall(self):
'''Test DeepStall Landing'''
# self.fly_deepstall_absolute()
self.fly_deepstall_relative()
def fly_deepstall_absolute(self):
self.start_subtest("DeepStall Relative Absolute")
deepstall_elevator_pwm = 1661
self.set_parameters({
"LAND_TYPE": 1,
"LAND_DS_ELEV_PWM": deepstall_elevator_pwm,
"RTL_AUTOLAND": 1,
})
self.load_mission("plane-deepstall-mission.txt")
self.change_mode("AUTO")
self.wait_ready_to_arm()
self.arm_vehicle()
self.progress("Waiting for deepstall messages")
# note that the following two don't necessarily happen in this
# order, but at very high speedups we may miss the elevator
# PWM if we first look for the text (due to the get_sim_time()
# in wait_servo_channel_value)
self.context_collect('STATUSTEXT')
# assume elevator is on channel 2:
self.wait_servo_channel_value(2, deepstall_elevator_pwm, timeout=240)
self.wait_text("Deepstall: Entry: ", check_context=True)
self.disarm_wait(timeout=120)
self.progress("Flying home")
self.set_current_waypoint(0, check_afterwards=False)
self.takeoff(10)
self.set_parameter("LAND_TYPE", 0)
self.fly_home_land_and_disarm()
def fly_deepstall_relative(self):
self.start_subtest("DeepStall Relative")
deepstall_elevator_pwm = 1661
self.set_parameters({
"LAND_TYPE": 1,
"LAND_DS_ELEV_PWM": deepstall_elevator_pwm,
"RTL_AUTOLAND": 1,
})
self.load_mission("plane-deepstall-relative-mission.txt")
self.change_mode("AUTO")
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_current_waypoint(4)
# assume elevator is on channel 2:
self.wait_servo_channel_value(2, deepstall_elevator_pwm, timeout=240)
self.progress("Waiting for stage DEEPSTALL_STAGE_LAND")
self.assert_receive_message(
'DEEPSTALL',
condition='DEEPSTALL.stage==6',
timeout=240,
)
self.progress("Reached stage DEEPSTALL_STAGE_LAND")
self.disarm_wait(timeout=120)
self.set_current_waypoint(0, check_afterwards=False)
self.progress("Flying home")
self.set_current_waypoint(0, check_afterwards=False)
self.takeoff(100)
self.set_parameter("LAND_TYPE", 0)
self.fly_home_land_and_disarm(timeout=240)
def SmartBattery(self):
'''Test smart battery logging etc'''
self.set_parameters({
"BATT_MONITOR": 16, # Maxell battery monitor
})
# Must reboot sitl after setting montior type for SMBus parameters to be set due to dynamic group
self.reboot_sitl()
self.set_parameters({
"BATT_I2C_BUS": 2, # specified in SIM_I2C.cpp
"BATT_I2C_ADDR": 11, # specified in SIM_I2C.cpp
})
self.reboot_sitl()
self.wait_ready_to_arm()
m = self.assert_receive_message('BATTERY_STATUS', timeout=10)
if m.voltages_ext[0] == 65536:
raise NotAchievedException("Flag value rather than voltage")
if abs(m.voltages_ext[0] - 1000) > 300:
raise NotAchievedException("Did not get good ext voltage (got=%f)" %
(m.voltages_ext[0],))
self.arm_vehicle()
self.delay_sim_time(5)
self.disarm_vehicle()
if not self.current_onboard_log_contains_message("BCL2"):
raise NotAchievedException("Expected BCL2 message")
def context_push_do_change_speed(self):
# the following lines ensure we revert these parameter values
# - DO_CHANGE_AIRSPEED is a permanent vehicle change!
self.context_push()
self.set_parameters({
"AIRSPEED_CRUISE": self.get_parameter("AIRSPEED_CRUISE"),
"MIN_GROUNDSPEED": self.get_parameter("MIN_GROUNDSPEED"),
"TRIM_THROTTLE": self.get_parameter("TRIM_THROTTLE"),
})
def DO_CHANGE_SPEED(self):
'''Test DO_CHANGE_SPEED command/item'''
self.set_parameters({
"RTL_AUTOLAND": 1,
})
self.context_push_do_change_speed()
self.DO_CHANGE_SPEED_mavlink_long()
self.context_pop()
self.set_current_waypoint(1)
self.zero_throttle()
self.context_push_do_change_speed()
self.DO_CHANGE_SPEED_mavlink_int()
self.context_pop()
self.context_push_do_change_speed()
self.DO_CHANGE_SPEED_mission()
self.context_pop()
def DO_CHANGE_SPEED_mission(self):
'''test DO_CHANGE_SPEED as a mission item'''
self.start_subtest("DO_CHANGE_SPEED_mission")
self.load_mission("mission.txt")
self.set_current_waypoint(1)
self.progress("Takeoff")
self.set_rc(3, 1000)
self.takeoff(alt=10)
self.set_rc(3, 1500)
self.start_subtest("Check initial speed")
self.change_mode('AUTO')
checks = [
(1, self.get_parameter("AIRSPEED_CRUISE")),
(3, 10),
(5, 20),
(7, 15),
]
for (current_waypoint, want_airspeed) in checks:
self.wait_current_waypoint(current_waypoint, timeout=150)
self.wait_airspeed(want_airspeed-1, want_airspeed+1, minimum_duration=5, timeout=120)
self.fly_home_land_and_disarm()
def DO_CHANGE_SPEED_mavlink_int(self):
self.DO_CHANGE_SPEED_mavlink(self.run_cmd_int)
def DO_CHANGE_SPEED_mavlink_long(self):
self.DO_CHANGE_SPEED_mavlink(self.run_cmd)
def DO_CHANGE_SPEED_mavlink(self, run_cmd_method):
'''test DO_CHANGE_SPEED as a mavlink command'''
self.progress("Takeoff")
self.takeoff(alt=100, mode="TAKEOFF", timeout=120)
self.set_rc(3, 1500)
# ensure we know what the airspeed is:
self.progress("Entering guided and flying somewhere constant")
self.change_mode("GUIDED")
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
p5=12345, # lat* 1e7
p6=12345, # lon* 1e7
p7=100 # alt
)
self.delay_sim_time(10)
self.progress("Ensuring initial speed is known and relatively constant")
initial_speed = 22.0
timeout = 15
self.wait_airspeed(initial_speed-1, initial_speed+1, minimum_duration=5, timeout=timeout)
self.start_subtest("Setting groundspeed")
for new_target_groundspeed in initial_speed + 5, initial_speed + 2:
run_cmd_method(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=1, # groundspeed
p2=new_target_groundspeed,
p3=-1, # throttle / no change
p4=0, # absolute values
)
self.wait_groundspeed(new_target_groundspeed-2, new_target_groundspeed+2, timeout=80, minimum_duration=5)
self.progress("Adding some wind, ensuring groundspeed holds")
self.set_parameter("SIM_WIND_SPD", 5)
self.delay_sim_time(5)
self.wait_groundspeed(new_target_groundspeed-2, new_target_groundspeed+2, timeout=40, minimum_duration=5)
self.set_parameter("SIM_WIND_SPD", 0)
# clear target groundspeed
run_cmd_method(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=1, # groundspeed
p2=0,
p3=-1, # throttle / no change
p4=0, # absolute values
)
self.start_subtest("Setting airspeed")
for new_target_airspeed in initial_speed - 5, initial_speed + 5:
run_cmd_method(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=0, # airspeed
p2=new_target_airspeed,
p3=-1, # throttle / no change
p4=0, # absolute values
)
self.wait_airspeed(new_target_airspeed-2, new_target_airspeed+2, minimum_duration=5)
self.context_push()
self.progress("Adding some wind, hoping groundspeed increases/decreases")
self.set_parameters({
"SIM_WIND_SPD": 7,
"SIM_WIND_DIR": 270,
})
self.delay_sim_time(5)
timeout = 10
tstart = self.get_sim_time()
while True:
if self.get_sim_time_cached() - tstart > timeout:
raise NotAchievedException("Did not achieve groundspeed delta")
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
delta = abs(m.airspeed - m.groundspeed)
want_delta = 5
self.progress("groundspeed and airspeed should be different (have=%f want=%f)" % (delta, want_delta))
if delta > want_delta:
break
self.context_pop()
# cancel minimum groundspeed:
run_cmd_method(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=0, # groundspeed
p2=-2, # return to default
p3=0, # throttle / no change
p4=0, # absolute values
)
# cancel airspeed:
run_cmd_method(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=1, # airspeed
p2=-2, # return to default
p3=0, # throttle / no change
p4=0, # absolute values
)
self.start_subtest("Setting throttle")
self.set_parameter('ARSPD_USE', 0) # setting throttle only effective without airspeed
for (set_throttle, expected_throttle) in (97, 79), (60, 51), (95, 77):
run_cmd_method(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=3, # throttle
p2=0,
p3=set_throttle, # throttle / no change
p4=0, # absolute values
)
self.wait_message_field_values('VFR_HUD', {
"throttle": expected_throttle,
}, minimum_duration=5, epsilon=2)
self.fly_home_land_and_disarm(timeout=240)
def fly_home_land_and_disarm(self, timeout=120):
filename = "flaps.txt"
self.progress("Using %s to fly home" % filename)
self.load_generic_mission(filename)
self.change_mode("AUTO")
# don't set current waypoint to 8 unless we're distant from it
# or we arrive instantly and never see it as our current
# waypoint:
self.wait_distance_to_waypoint(8, 100, 10000000)
self.set_current_waypoint(8)
# TODO: reflect on file to find this magic waypoint number?
# self.wait_waypoint(7, num_wp-1, timeout=500) # we
# tend to miss the final waypoint by a fair bit, and
# this is probably too noisy anyway?
self.wait_disarmed(timeout=timeout)
def TestFlaps(self):
"""Test flaps functionality."""
filename = "flaps.txt"
self.context_push()
ex = None
try:
flaps_ch = 5
flaps_ch_min = 1000
flaps_ch_trim = 1500
flaps_ch_max = 2000
servo_ch = 5
servo_ch_min = 1200
servo_ch_trim = 1300
servo_ch_max = 1800
self.set_parameters({
"SERVO%u_FUNCTION" % servo_ch: 3, # flapsauto
"RC%u_OPTION" % flaps_ch: 208, # Flaps RCx_OPTION
"LAND_FLAP_PERCNT": 50,
"LOG_DISARMED": 1,
"RTL_AUTOLAND": 1,
"RC%u_MIN" % flaps_ch: flaps_ch_min,
"RC%u_MAX" % flaps_ch: flaps_ch_max,
"RC%u_TRIM" % flaps_ch: flaps_ch_trim,
"SERVO%u_MIN" % servo_ch: servo_ch_min,
"SERVO%u_MAX" % servo_ch: servo_ch_max,
"SERVO%u_TRIM" % servo_ch: servo_ch_trim,
})
self.progress("check flaps are not deployed")
self.set_rc(flaps_ch, flaps_ch_min)
self.wait_servo_channel_value(servo_ch, servo_ch_min, timeout=3)
self.progress("deploy the flaps")
self.set_rc(flaps_ch, flaps_ch_max)
tstart = self.get_sim_time()
self.wait_servo_channel_value(servo_ch, servo_ch_max)
tstop = self.get_sim_time_cached()
delta_time = tstop - tstart
delta_time_min = 0.5
delta_time_max = 1.5
if delta_time < delta_time_min or delta_time > delta_time_max:
raise NotAchievedException((
"Flaps Slew not working (%f seconds)" % (delta_time,)))
self.progress("undeploy flaps")
self.set_rc(flaps_ch, flaps_ch_min)
self.wait_servo_channel_value(servo_ch, servo_ch_min)
self.progress("Flying mission %s" % filename)
self.load_mission(filename)
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
last_mission_current_msg = 0
last_seq = None
while self.armed():
m = self.mav.recv_match(type='MISSION_CURRENT', blocking=True)
time_delta = (self.get_sim_time_cached() -
last_mission_current_msg)
if (time_delta > 1 or m.seq != last_seq):
dist = None
x = self.mav.messages.get("NAV_CONTROLLER_OUTPUT", None)
if x is not None:
dist = x.wp_dist
self.progress("MISSION_CURRENT.seq=%u (dist=%s)" %
(m.seq, str(dist)))
last_mission_current_msg = self.get_sim_time_cached()
last_seq = m.seq
# flaps should undeploy at the end
self.wait_servo_channel_value(servo_ch, servo_ch_min, timeout=30)
# do a short flight in FBWA, watching for flaps
# self.mavproxy.send('switch 4\n')
# self.wait_mode('FBWA')
# self.delay_sim_time(10)
# self.mavproxy.send('switch 6\n')
# self.wait_mode('MANUAL')
# self.delay_sim_time(10)
self.progress("Flaps OK")
except Exception as e:
self.print_exception_caught(e)
ex = e
self.context_pop()
if ex:
if self.armed():
self.disarm_vehicle()
raise ex
def TestRCRelay(self):
'''Test Relay RC Channel Option'''
self.set_parameters({
"RELAY1_FUNCTION": 1, # Enable relay as a standard relay pin
"RC12_OPTION": 28 # Relay On/Off
})
self.set_rc(12, 1000)
self.reboot_sitl() # needed for RC12_OPTION and RELAY1_FUNCTION to take effect
off = self.get_parameter("SIM_PIN_MASK")
if off:
raise PreconditionFailedException("SIM_MASK_PIN off")
# allow time for the RC library to register initial value:
self.delay_sim_time(1)
self.set_rc(12, 2000)
self.wait_heartbeat()
self.wait_heartbeat()
on = self.get_parameter("SIM_PIN_MASK")
if not on:
raise NotAchievedException("SIM_PIN_MASK doesn't reflect ON")
self.set_rc(12, 1000)
self.wait_heartbeat()
self.wait_heartbeat()
off = self.get_parameter("SIM_PIN_MASK")
if off:
raise NotAchievedException("SIM_PIN_MASK doesn't reflect OFF")
def TestRCCamera(self):
'''Test RC Option - Camera Trigger'''
self.set_parameter("RC12_OPTION", 9) # CameraTrigger
self.set_parameter("CAM1_TYPE", 1) # Camera with servo trigger
self.reboot_sitl() # needed for RC12_OPTION to take effect
x = self.mav.messages.get("CAMERA_FEEDBACK", None)
if x is not None:
raise PreconditionFailedException("Receiving CAMERA_FEEDBACK?!")
self.set_rc(12, 2000)
tstart = self.get_sim_time()
while self.get_sim_time_cached() - tstart < 10:
x = self.mav.messages.get("CAMERA_FEEDBACK", None)
if x is not None:
break
self.wait_heartbeat()
self.set_rc(12, 1000)
if x is None:
raise NotAchievedException("No CAMERA_FEEDBACK message received")
self.wait_ready_to_arm()
original_alt = self.get_altitude()
takeoff_alt = 30
self.takeoff(takeoff_alt)
self.set_rc(12, 2000)
self.delay_sim_time(1)
self.set_rc(12, 1000)
x = self.mav.messages.get("CAMERA_FEEDBACK", None)
if abs(x.alt_rel - takeoff_alt) > 10:
raise NotAchievedException("Bad relalt (want=%f vs got=%f)" % (takeoff_alt, x.alt_rel))
if abs(x.alt_msl - (original_alt+30)) > 10:
raise NotAchievedException("Bad absalt (want=%f vs got=%f)" % (original_alt+30, x.alt_msl))
self.fly_home_land_and_disarm()
def ThrottleFailsafe(self):
'''Fly throttle failsafe'''
self.change_mode('MANUAL')
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
receiver_bit = mavutil.mavlink.MAV_SYS_STATUS_SENSOR_RC_RECEIVER
self.progress("Testing receiver enabled")
if (not (m.onboard_control_sensors_enabled & receiver_bit)):
raise PreconditionFailedException()
self.progress("Testing receiver present")
if (not (m.onboard_control_sensors_present & receiver_bit)):
raise PreconditionFailedException()
self.progress("Testing receiver health")
if (not (m.onboard_control_sensors_health & receiver_bit)):
raise PreconditionFailedException()
self.progress("Ensure we know original throttle value")
self.wait_rc_channel_value(3, 1000)
self.set_parameter("THR_FS_VALUE", 960)
self.progress("Failing receiver (throttle-to-950)")
self.context_collect("HEARTBEAT")
self.set_parameter("SIM_RC_FAIL", 2) # throttle-to-950
self.wait_mode('RTL') # long failsafe
if (self.get_mode_from_mode_mapping("CIRCLE") not in
[x.custom_mode for x in self.context_stop_collecting("HEARTBEAT")]):
raise NotAchievedException("Did not go via circle mode")
self.progress("Ensure we've had our throttle squashed to 950")
self.wait_rc_channel_value(3, 950)
self.do_timesync_roundtrip()
m = self.assert_receive_message('SYS_STATUS')
self.progress("Got (%s)" % str(m))
self.progress("Testing receiver enabled")
if (not (m.onboard_control_sensors_enabled & receiver_bit)):
raise NotAchievedException("Receiver not enabled")
self.progress("Testing receiver present")
if (not (m.onboard_control_sensors_present & receiver_bit)):
raise NotAchievedException("Receiver not present")
# skip this until RC is fixed
# self.progress("Testing receiver health")
# if (m.onboard_control_sensors_health & receiver_bit):
# raise NotAchievedException("Sensor healthy when it shouldn't be")
self.set_parameter("SIM_RC_FAIL", 0)
# have to allow time for RC to be fetched from SITL
self.delay_sim_time(0.5)
self.do_timesync_roundtrip()
m = self.assert_receive_message('SYS_STATUS')
self.progress("Testing receiver enabled")
if (not (m.onboard_control_sensors_enabled & receiver_bit)):
raise NotAchievedException("Receiver not enabled")
self.progress("Testing receiver present")
if (not (m.onboard_control_sensors_present & receiver_bit)):
raise NotAchievedException("Receiver not present")
self.progress("Testing receiver health")
if (not (m.onboard_control_sensors_health & receiver_bit)):
raise NotAchievedException("Receiver not healthy2")
self.change_mode('MANUAL')
self.progress("Failing receiver (no-pulses)")
self.context_collect("HEARTBEAT")
self.set_parameter("SIM_RC_FAIL", 1) # no-pulses
self.wait_mode('RTL') # long failsafe
if (self.get_mode_from_mode_mapping("CIRCLE") not in
[x.custom_mode for x in self.context_stop_collecting("HEARTBEAT")]):
raise NotAchievedException("Did not go via circle mode")
self.do_timesync_roundtrip()
m = self.assert_receive_message('SYS_STATUS')
self.progress("Got (%s)" % str(m))
self.progress("Testing receiver enabled")
if (not (m.onboard_control_sensors_enabled & receiver_bit)):
raise NotAchievedException("Receiver not enabled")
self.progress("Testing receiver present")
if (not (m.onboard_control_sensors_present & receiver_bit)):
raise NotAchievedException("Receiver not present")
self.progress("Testing receiver health")
if (m.onboard_control_sensors_health & receiver_bit):
raise NotAchievedException("Sensor healthy when it shouldn't be")
self.progress("Making RC work again")
self.set_parameter("SIM_RC_FAIL", 0)
# have to allow time for RC to be fetched from SITL
self.progress("Giving receiver time to recover")
self.delay_sim_time(0.5)
self.do_timesync_roundtrip()
m = self.assert_receive_message('SYS_STATUS')
self.progress("Testing receiver enabled")
if (not (m.onboard_control_sensors_enabled & receiver_bit)):
raise NotAchievedException("Receiver not enabled")
self.progress("Testing receiver present")
if (not (m.onboard_control_sensors_present & receiver_bit)):
raise NotAchievedException("Receiver not present")
self.progress("Testing receiver health")
if (not (m.onboard_control_sensors_health & receiver_bit)):
raise NotAchievedException("Receiver not healthy")
self.change_mode('MANUAL')
self.progress("Ensure long failsafe can trigger when short failsafe disabled")
self.context_push()
self.context_collect("STATUSTEXT")
ex = None
try:
self.set_parameters({
"FS_SHORT_ACTN": 3, # 3 means disabled
"SIM_RC_FAIL": 1,
})
self.wait_statustext("Long failsafe on", check_context=True)
self.wait_mode("RTL")
# self.context_clear_collection("STATUSTEXT")
self.set_parameter("SIM_RC_FAIL", 0)
self.wait_text("Long Failsafe Cleared", check_context=True)
self.change_mode("MANUAL")
self.progress("Trying again with THR_FS_VALUE")
self.set_parameters({
"THR_FS_VALUE": 960,
"SIM_RC_FAIL": 2,
})
self.wait_statustext("Long Failsafe on", check_context=True)
self.wait_mode("RTL")
except Exception as e:
self.print_exception_caught(e)
ex = e
self.context_pop()
if ex is not None:
raise ex
self.start_subtest("Not use RC throttle input when THR_FAILSAFE==2")
self.takeoff(100)
self.set_rc(3, 1800)
self.set_rc(1, 2000)
self.wait_attitude(desroll=45, timeout=1)
self.context_push()
self.set_parameters({
"THR_FAILSAFE": 2,
"SIM_RC_FAIL": 1, # no pulses
})
self.delay_sim_time(1)
self.wait_attitude(desroll=0, timeout=5)
self.assert_servo_channel_value(3, self.get_parameter("RC3_MIN"))
self.set_parameters({
"SIM_RC_FAIL": 0, # fix receiver
})
self.zero_throttle()
self.disarm_vehicle(force=True)
self.context_pop()
self.reboot_sitl()
def ThrottleFailsafeFence(self):
'''Fly fence survives throttle failsafe'''
fence_bit = mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE
self.progress("Checking fence is not present before being configured")
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
self.progress("Got (%s)" % str(m))
if (m.onboard_control_sensors_enabled & fence_bit):
raise NotAchievedException("Fence enabled before being configured")
self.change_mode('MANUAL')
self.wait_ready_to_arm()
self.load_fence("CMAC-fence.txt")
self.set_parameter("RC7_OPTION", 11) # AC_Fence uses Aux switch functionality
self.set_parameter("FENCE_ACTION", 4) # Fence action Brake
self.set_rc_from_map({
3: 1000,
7: 2000,
}) # Turn fence on with aux function
m = self.mav.recv_match(type='FENCE_STATUS', blocking=True, timeout=2)
self.progress("Got (%s)" % str(m))
if m is None:
raise NotAchievedException("Got FENCE_STATUS unexpectedly")
self.progress("Checking fence is initially OK")
self.wait_sensor_state(mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE,
present=True,
enabled=True,
healthy=True,
verbose=True,
timeout=30)
self.set_parameter("THR_FS_VALUE", 960)
self.progress("Failing receiver (throttle-to-950)")
self.set_parameter("SIM_RC_FAIL", 2) # throttle-to-950
self.wait_mode("CIRCLE")
self.delay_sim_time(1) # give
self.do_timesync_roundtrip()
self.progress("Checking fence is OK after receiver failure (bind-values)")
fence_bit = mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE
m = self.assert_receive_message('SYS_STATUS')
if (not (m.onboard_control_sensors_enabled & fence_bit)):
raise NotAchievedException("Fence not enabled after RC fail")
self.do_fence_disable() # Ensure the fence is disabled after test
def GCSFailsafe(self):
'''Ensure Long-Failsafe works on GCS loss'''
self.start_subtest("Test Failsafe: RTL")
self.load_sample_mission()
self.set_parameters({
"FS_GCS_ENABL": 1,
"FS_LONG_ACTN": 1,
"RTL_AUTOLAND": 1,
"SYSID_MYGCS": self.mav.source_system,
})
self.takeoff()
self.change_mode('LOITER')
self.progress("Disconnecting GCS")
self.set_heartbeat_rate(0)
self.wait_mode("RTL", timeout=10)
self.set_heartbeat_rate(self.speedup)
self.end_subtest("Completed RTL Failsafe test")
self.start_subtest("Test Failsafe: FBWA Glide")
self.set_parameters({
"FS_LONG_ACTN": 2,
})
self.change_mode('AUTO')
self.progress("Disconnecting GCS")
self.set_heartbeat_rate(0)
self.wait_mode("FBWA", timeout=10)
self.set_heartbeat_rate(self.speedup)
self.end_subtest("Completed FBWA Failsafe test")
self.start_subtest("Test Failsafe: Deploy Parachute")
self.load_mission("plane-parachute-mission.txt")
self.set_current_waypoint(1)
self.set_parameters({
"CHUTE_ENABLED": 1,
"CHUTE_TYPE": 10,
"SERVO9_FUNCTION": 27,
"SIM_PARA_ENABLE": 1,
"SIM_PARA_PIN": 9,
"FS_LONG_ACTN": 3,
})
self.change_mode("AUTO")
self.progress("Disconnecting GCS")
self.set_heartbeat_rate(0)
self.wait_statustext("BANG", timeout=60)
self.set_heartbeat_rate(self.speedup)
self.disarm_vehicle(force=True)
self.reboot_sitl()
self.end_subtest("Completed Parachute Failsafe test")
def TestGripperMission(self):
'''Test Gripper mission items'''
self.context_push()
ex = None
try:
self.set_parameter("RTL_AUTOLAND", 1)
self.load_mission("plane-gripper-mission.txt")
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_statustext("Gripper Grabbed", timeout=60)
self.wait_statustext("Gripper Released", timeout=60)
self.wait_statustext("Auto disarmed", timeout=60)
except Exception as e:
self.print_exception_caught(e)
ex = e
self.context_pop()
if ex is not None:
raise ex
def assert_fence_sys_status(self, present, enabled, health):
self.delay_sim_time(1)
self.do_timesync_roundtrip()
m = self.assert_receive_message('SYS_STATUS', timeout=1)
tests = [
("present", present, m.onboard_control_sensors_present),
("enabled", enabled, m.onboard_control_sensors_enabled),
("health", health, m.onboard_control_sensors_health),
]
bit = mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE
for test in tests:
(name, want, field) = test
got = (field & bit) != 0
if want != got:
raise NotAchievedException("fence status incorrect; %s want=%u got=%u" %
(name, want, got))
def wait_circling_point_with_radius(self, loc, want_radius, epsilon=5.0, min_circle_time=5, timeout=120):
on_radius_start_heading = None
average_radius = 0.0
circle_time_start = 0
done_time = False
done_angle = False
tstart = self.get_sim_time()
while True:
if self.get_sim_time() - tstart > timeout:
raise AutoTestTimeoutException("Did not get onto circle")
here = self.mav.location()
got_radius = self.get_distance(loc, here)
average_radius = 0.95*average_radius + 0.05*got_radius
on_radius = abs(got_radius - want_radius) < epsilon
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
heading = m.heading
on_string = "off"
got_angle = ""
if on_radius_start_heading is not None:
got_angle = "%0.2f" % abs(on_radius_start_heading - heading) # FIXME
on_string = "on"
want_angle = 180 # we don't actually get this (angle-substraction issue. But we get enough...
self.progress("wait-circling: got-r=%0.2f want-r=%f avg-r=%f %s want-a=%0.1f got-a=%s" %
(got_radius, want_radius, average_radius, on_string, want_angle, got_angle))
if on_radius:
if on_radius_start_heading is None:
on_radius_start_heading = heading
average_radius = got_radius
circle_time_start = self.get_sim_time()
continue
if abs(on_radius_start_heading - heading) > want_angle: # FIXME
done_angle = True
if self.get_sim_time() - circle_time_start > min_circle_time:
done_time = True
if done_time and done_angle:
return
continue
if on_radius_start_heading is not None:
average_radius = 0.0
on_radius_start_heading = None
circle_time_start = 0
def MODE_SWITCH_RESET(self):
'''test the MODE_SWITCH_RESET auxiliary function'''
self.set_parameters({
"RC9_OPTION": 96,
})
self.progress("Using RC to change modes")
self.set_rc(8, 1500)
self.wait_mode('FBWA')
self.progress("Killing RC to engage RC failsafe")
self.set_parameter('SIM_RC_FAIL', 1)
self.wait_mode('RTL')
self.progress("Reinstating RC")
self.set_parameter('SIM_RC_FAIL', 0)
self.progress("Ensuring we don't automatically revert mode")
self.delay_sim_time(2)
self.assert_mode_is('RTL')
self.progress("Ensuring MODE_SWITCH_RESET switch resets to pre-failsafe mode")
self.set_rc(9, 2000)
self.wait_mode('FBWA')
def FenceStatic(self):
'''Test Basic Fence Functionality'''
ex = None
try:
self.progress("Checking for bizarre healthy-when-not-present-or-enabled")
self.set_parameter("FENCE_TYPE", 4) # Start by only setting polygon fences, otherwise fence will report present
self.assert_fence_sys_status(False, False, True)
self.load_fence("CMAC-fence.txt")
m = self.mav.recv_match(type='FENCE_STATUS', blocking=True, timeout=2)
if m is not None:
raise NotAchievedException("Got FENCE_STATUS unexpectedly")
self.set_parameter("FENCE_ACTION", 0) # report only
self.assert_fence_sys_status(True, False, True)
self.set_parameter("FENCE_ACTION", 1) # RTL
self.assert_fence_sys_status(True, False, True)
self.do_fence_enable()
self.assert_fence_sys_status(True, True, True)
m = self.assert_receive_message('FENCE_STATUS', timeout=2)
if m.breach_status:
raise NotAchievedException("Breached fence unexpectedly (%u)" %
(m.breach_status))
self.do_fence_disable()
self.assert_fence_sys_status(True, False, True)
self.set_parameter("FENCE_ACTION", 1)
self.assert_fence_sys_status(True, False, True)
self.set_parameter("FENCE_ACTION", 0)
self.assert_fence_sys_status(True, False, True)
self.clear_fence()
if self.get_parameter("FENCE_TOTAL") != 0:
raise NotAchievedException("Expected zero points remaining")
self.assert_fence_sys_status(False, False, True)
self.progress("Trying to enable fence with no points")
self.do_fence_enable(want_result=mavutil.mavlink.MAV_RESULT_FAILED)
# test a rather unfortunate behaviour:
self.progress("Killing a live fence with fence-clear")
self.load_fence("CMAC-fence.txt")
self.set_parameter("FENCE_ACTION", 1) # AC_FENCE_ACTION_RTL_AND_LAND == 1. mavutil.mavlink.FENCE_ACTION_RTL == 4
self.do_fence_enable()
self.assert_fence_sys_status(True, True, True)
self.clear_fence()
self.wait_sensor_state(mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE, False, False, True)
if self.get_parameter("FENCE_TOTAL") != 0:
raise NotAchievedException("Expected zero points remaining")
self.assert_fence_sys_status(False, False, True)
self.do_fence_disable()
# ensure that a fence is present if it is tin can, min alt or max alt
self.progress("Test other fence types (tin-can, min alt, max alt")
self.set_parameter("FENCE_TYPE", 1) # max alt
self.assert_fence_sys_status(True, False, True)
self.set_parameter("FENCE_TYPE", 8) # min alt
self.assert_fence_sys_status(True, False, True)
self.set_parameter("FENCE_TYPE", 2) # tin can
self.assert_fence_sys_status(True, False, True)
# Test cannot arm if outside of fence and fence is enabled
self.progress("Test Arming while vehicle below FENCE_ALT_MIN")
default_fence_alt_min = self.get_parameter("FENCE_ALT_MIN")
self.set_parameter("FENCE_ALT_MIN", 50)
self.set_parameter("FENCE_TYPE", 8) # Enables minimum altitude breaches
self.do_fence_enable()
self.delay_sim_time(2) # Allow breach to propagate
self.assert_fence_enabled()
self.try_arm(False, "vehicle outside fence")
self.do_fence_disable()
self.set_parameter("FENCE_ALT_MIN", default_fence_alt_min)
# Test arming outside inclusion zone
self.progress("Test arming while vehicle outside of inclusion zone")
self.set_parameter("FENCE_TYPE", 4) # Enables polygon fence types
locs = [
mavutil.location(1.000, 1.000, 0, 0),
mavutil.location(1.000, 1.001, 0, 0),
mavutil.location(1.001, 1.001, 0, 0),
mavutil.location(1.001, 1.000, 0, 0)
]
self.upload_fences_from_locations(
mavutil.mavlink.MAV_CMD_NAV_FENCE_POLYGON_VERTEX_INCLUSION,
[
locs
]
)
self.delay_sim_time(10) # let fence check run so it loads-from-eeprom
self.do_fence_enable()
self.assert_fence_enabled()
self.delay_sim_time(2) # Allow breach to propagate
self.try_arm(False, "vehicle outside fence")
self.do_fence_disable()
self.clear_fence()
self.progress("Test arming while vehicle inside exclusion zone")
self.set_parameter("FENCE_TYPE", 4) # Enables polygon fence types
home_loc = self.mav.location()
locs = [
mavutil.location(home_loc.lat - 0.001, home_loc.lng - 0.001, 0, 0),
mavutil.location(home_loc.lat - 0.001, home_loc.lng + 0.001, 0, 0),
mavutil.location(home_loc.lat + 0.001, home_loc.lng + 0.001, 0, 0),
mavutil.location(home_loc.lat + 0.001, home_loc.lng - 0.001, 0, 0),
]
self.upload_fences_from_locations(
mavutil.mavlink.MAV_CMD_NAV_FENCE_POLYGON_VERTEX_EXCLUSION,
[
locs
]
)
self.delay_sim_time(10) # let fence check run so it loads-from-eeprom
self.do_fence_enable()
self.assert_fence_enabled()
self.delay_sim_time(2) # Allow breach to propagate
self.try_arm(False, "vehicle outside fence")
self.do_fence_disable()
self.clear_fence()
except Exception as e:
self.print_exception_caught(e)
ex = e
self.clear_fence()
if ex is not None:
raise ex
def test_fence_breach_circle_at(self, loc, disable_on_breach=False):
ex = None
try:
self.load_fence("CMAC-fence.txt")
want_radius = 100
# when ArduPlane is fixed, remove this fudge factor
REALLY_BAD_FUDGE_FACTOR = 1.16
expected_radius = REALLY_BAD_FUDGE_FACTOR * want_radius
self.set_parameters({
"RTL_RADIUS": want_radius,
"NAVL1_LIM_BANK": 60,
"FENCE_ACTION": 1, # AC_FENCE_ACTION_RTL_AND_LAND == 1. mavutil.mavlink.FENCE_ACTION_RTL == 4
})
self.wait_ready_to_arm() # need an origin to load fence
self.do_fence_enable()
self.assert_fence_sys_status(True, True, True)
self.takeoff(alt=45, alt_max=300)
tstart = self.get_sim_time()
while True:
if self.get_sim_time() - tstart > 30:
raise NotAchievedException("Did not breach fence")
m = self.assert_receive_message('FENCE_STATUS', timeout=2)
if m.breach_status == 0:
continue
# we've breached; check our state;
if m.breach_type != mavutil.mavlink.FENCE_BREACH_BOUNDARY:
raise NotAchievedException("Unexpected breach type %u" %
(m.breach_type,))
if m.breach_count == 0:
raise NotAchievedException("Unexpected breach count %u" %
(m.breach_count,))
self.assert_fence_sys_status(True, True, False)
break
if disable_on_breach:
self.do_fence_disable()
self.wait_circling_point_with_radius(loc, expected_radius)
self.disarm_vehicle(force=True)
self.reboot_sitl()
except Exception as e:
self.print_exception_caught(e)
ex = e
self.clear_fence()
if ex is not None:
raise ex
def FenceRTL(self):
'''Test Fence RTL'''
self.progress("Testing FENCE_ACTION_RTL no rally point")
# have to disable the fence once we've breached or we breach
# it as part of the loiter-at-home!
self.test_fence_breach_circle_at(self.home_position_as_mav_location(),
disable_on_breach=True)
def FenceRTLRally(self):
'''Test Fence RTL Rally'''
ex = None
target_system = 1
target_component = 1
try:
self.progress("Testing FENCE_ACTION_RTL with rally point")
self.wait_ready_to_arm()
loc = self.home_relative_loc_ne(50, -50)
self.set_parameter("RALLY_TOTAL", 1)
self.mav.mav.rally_point_send(target_system,
target_component,
0, # sequence number
1, # total count
int(loc.lat * 1e7),
int(loc.lng * 1e7),
15,
0, # "break" alt?!
0, # "land dir"
0) # flags
self.delay_sim_time(1)
if self.mavproxy is not None:
self.mavproxy.send("rally list\n")
self.test_fence_breach_circle_at(loc)
except Exception as e:
self.print_exception_caught(e)
ex = e
self.clear_mission(mavutil.mavlink.MAV_MISSION_TYPE_RALLY)
if ex is not None:
raise ex
def FenceRetRally(self):
""" Tests the FENCE_RET_RALLY flag, either returning to fence return point,
or rally point """
target_system = 1
target_component = 1
self.progress("Testing FENCE_ACTION_RTL with fence rally point")
self.wait_ready_to_arm()
self.homeloc = self.mav.location()
# Grab a location for fence return point, and upload it.
fence_loc = self.home_position_as_mav_location()
self.location_offset_ne(fence_loc, 50, 50)
fence_return_mission_items = [
self.mav.mav.mission_item_int_encode(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL_INT,
mavutil.mavlink.MAV_CMD_NAV_FENCE_RETURN_POINT,
0, # current
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
int(fence_loc.lat * 1e7), # latitude
int(fence_loc.lng * 1e7), # longitude
0, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_FENCE
)
]
self.upload_using_mission_protocol(mavutil.mavlink.MAV_MISSION_TYPE_FENCE,
fence_return_mission_items)
self.delay_sim_time(1)
# Grab a location for rally point, and upload it.
rally_loc = self.home_relative_loc_ne(-50, 50)
self.set_parameter("RALLY_TOTAL", 1)
self.mav.mav.rally_point_send(target_system,
target_component,
0, # sequence number
1, # total count
int(rally_loc.lat * 1e7),
int(rally_loc.lng * 1e7),
15,
0, # "break" alt?!
0, # "land dir"
0) # flags
self.delay_sim_time(1)
return_radius = 100
return_alt = 80
self.set_parameters({
"RTL_RADIUS": return_radius,
"FENCE_ACTION": 6, # Set Fence Action to Guided
"FENCE_TYPE": 8, # Only use fence floor
"FENCE_RET_ALT": return_alt,
})
self.do_fence_enable()
self.assert_fence_enabled()
self.takeoff(alt=50, alt_max=300)
# Trigger fence breach, fly to rally location
self.set_parameters({
"FENCE_RET_RALLY": 1,
"FENCE_ALT_MIN": 60,
})
self.wait_circling_point_with_radius(rally_loc, return_radius)
self.set_parameter("FENCE_ALT_MIN", 0) # Clear fence breach
# 10 second fence min retrigger time
self.delay_sim_time(15)
# Fly up before re-triggering fence breach. Fly to fence return point
self.change_altitude(self.homeloc.alt+30)
self.set_parameters({
"FENCE_RET_RALLY": 0,
"FENCE_ALT_MIN": 60,
})
self.wait_altitude(altitude_min=return_alt-3,
altitude_max=return_alt+3,
relative=True)
self.wait_circling_point_with_radius(fence_loc, return_radius)
self.do_fence_disable() # Disable fence so we can land
self.fly_home_land_and_disarm() # Pack it up, we're going home.
def TerrainRally(self):
""" Tests terrain follow with a rally point """
self.context_push()
self.install_terrain_handlers_context()
def terrain_following_above_80m(mav, m):
if m.get_type() == 'TERRAIN_REPORT':
if m.current_height < 50:
raise NotAchievedException(
"TERRAIN_REPORT.current_height below 50m %fm" % m.current_height)
if m.get_type() == 'VFR_HUD':
if m.groundspeed < 2:
raise NotAchievedException("hit ground")
def terrain_wait_path(loc1, loc2, steps):
'''wait till we have terrain for N steps from loc1 to loc2'''
tstart = self.get_sim_time_cached()
self.progress("Waiting for terrain data")
while True:
now = self.get_sim_time_cached()
if now - tstart > 60:
raise NotAchievedException("Did not get correct required terrain")
for i in range(steps):
lat = loc1.lat + i * (loc2.lat-loc1.lat)/steps
lon = loc1.lng + i * (loc2.lng-loc1.lng)/steps
self.mav.mav.terrain_check_send(int(lat*1.0e7), int(lon*1.0e7))
report = self.assert_receive_message('TERRAIN_REPORT', timeout=60)
self.progress("Terrain pending=%u" % report.pending)
if report.pending == 0:
break
self.progress("Got required terrain")
self.wait_ready_to_arm()
self.homeloc = self.mav.location()
guided_loc = mavutil.location(-35.39723762, 149.07284612, self.homeloc.alt+99.0, 0)
rally_loc = mavutil.location(-35.3654952000, 149.1558698000, self.homeloc.alt+100, 0)
terrain_wait_path(self.homeloc, rally_loc, 10)
# set a rally point to the west of home
self.upload_rally_points_from_locations([rally_loc])
self.set_parameter("TKOFF_ALT", 100)
self.change_mode("TAKEOFF")
self.wait_ready_to_arm()
self.arm_vehicle()
self.set_parameter("TERRAIN_FOLLOW", 1)
self.wait_altitude(90, 120, timeout=30, relative=True)
self.progress("Done takeoff")
self.install_message_hook_context(terrain_following_above_80m)
self.change_mode("GUIDED")
self.do_reposition(guided_loc, frame=mavutil.mavlink.MAV_FRAME_GLOBAL_TERRAIN_ALT)
self.progress("Flying to guided location")
self.wait_location(
guided_loc,
accuracy=200,
timeout=600,
height_accuracy=10,
)
self.progress("Reached guided location")
self.set_parameter("RALLY_LIMIT_KM", 50)
self.change_mode("RTL")
self.progress("Flying to rally point")
self.wait_location(
rally_loc,
accuracy=200,
timeout=600,
height_accuracy=10,
)
self.progress("Reached rally point with TERRAIN_FOLLOW")
# Fly back to guided location
self.change_mode("GUIDED")
self.do_reposition(guided_loc, frame=mavutil.mavlink.MAV_FRAME_GLOBAL_TERRAIN_ALT)
self.progress("Flying to back to guided location")
# Disable terrain following and re-load rally point with relative to terrain altitude
self.set_parameter("TERRAIN_FOLLOW", 0)
rally_item = [self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_NAV_RALLY_POINT,
x=int(rally_loc.lat*1e7),
y=int(rally_loc.lng*1e7),
z=rally_loc.alt,
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_TERRAIN_ALT,
mission_type=mavutil.mavlink.MAV_MISSION_TYPE_RALLY
)]
self.correct_wp_seq_numbers(rally_item)
self.check_rally_upload_download(rally_item)
# Once back at guided location re-trigger RTL
self.wait_location(
guided_loc,
accuracy=200,
timeout=600,
height_accuracy=10,
)
self.change_mode("RTL")
self.progress("Flying to rally point")
self.wait_location(
rally_loc,
accuracy=200,
timeout=600,
height_accuracy=10,
)
self.progress("Reached rally point with terrain alt frame")
self.context_pop()
self.disarm_vehicle(force=True)
self.reboot_sitl()
def Parachute(self):
'''Test Parachute'''
self.set_rc(9, 1000)
self.set_parameters({
"CHUTE_ENABLED": 1,
"CHUTE_TYPE": 10,
"SERVO9_FUNCTION": 27,
"SIM_PARA_ENABLE": 1,
"SIM_PARA_PIN": 9,
})
self.load_mission("plane-parachute-mission.txt")
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_statustext("BANG", timeout=60)
self.disarm_vehicle(force=True)
self.reboot_sitl()
def ParachuteSinkRate(self):
'''Test Parachute (SinkRate triggering)'''
self.set_rc(9, 1000)
self.set_parameters({
"CHUTE_ENABLED": 1,
"CHUTE_TYPE": 10,
"SERVO9_FUNCTION": 27,
"SIM_PARA_ENABLE": 1,
"SIM_PARA_PIN": 9,
"CHUTE_CRT_SINK": 9,
})
self.progress("Takeoff")
self.takeoff(alt=300)
self.progress("Diving")
self.set_rc(2, 2000)
self.wait_statustext("BANG", timeout=60)
self.disarm_vehicle(force=True)
self.reboot_sitl()
def run_subtest(self, desc, func):
self.start_subtest(desc)
func()
def fly_ahrs2_test(self):
'''check secondary estimator is looking OK'''
ahrs2 = self.mav.recv_match(type='AHRS2', blocking=True, timeout=1)
if ahrs2 is None:
raise NotAchievedException("Did not receive AHRS2 message")
self.progress("AHRS2: %s" % str(ahrs2))
# check location
gpi = self.mav.recv_match(
type='GLOBAL_POSITION_INT',
blocking=True,
timeout=5
)
if gpi is None:
raise NotAchievedException("Did not receive GLOBAL_POSITION_INT message")
self.progress("GPI: %s" % str(gpi))
if self.get_distance_int(gpi, ahrs2) > 10:
raise NotAchievedException("Secondary location looks bad")
self.check_attitudes_match()
def MainFlight(self):
'''Lots of things in one flight'''
self.change_mode('MANUAL')
self.progress("Asserting we do support transfer of fence via mission item protocol")
self.assert_capability(mavutil.mavlink.MAV_PROTOCOL_CAPABILITY_MISSION_FENCE)
# grab home position:
self.mav.recv_match(type='HOME_POSITION', blocking=True)
self.homeloc = self.mav.location()
self.run_subtest("Takeoff", self.takeoff)
self.run_subtest("Set Attitude Target", self.set_attitude_target)
self.run_subtest("Fly left circuit", self.fly_left_circuit)
self.run_subtest("Left roll", lambda: self.axial_left_roll(1))
self.run_subtest("Inside loop", self.inside_loop)
self.run_subtest("Stablize test", self.test_stabilize)
self.run_subtest("ACRO test", self.test_acro)
self.run_subtest("FBWB test", self.test_FBWB)
self.run_subtest("CRUISE test", lambda: self.test_FBWB(mode='CRUISE'))
self.run_subtest("RTL test", self.fly_RTL)
self.run_subtest("LOITER test", self.fly_LOITER)
self.run_subtest("CIRCLE test", self.fly_CIRCLE)
self.run_subtest("AHRS2 test", self.fly_ahrs2_test)
self.run_subtest("Mission test",
lambda: self.fly_mission("ap1.txt", strict=False))
def PitotBlockage(self):
'''Test detection and isolation of a blocked pitot tube'''
self.set_parameters({
"ARSPD_OPTIONS": 15,
"ARSPD_USE": 1,
"SIM_WIND_SPD": 7,
"SIM_WIND_DIR": 0,
"ARSPD_WIND_MAX": 15,
})
self.takeoff(alt=50, mode='TAKEOFF')
# simulate the effect of a blocked pitot tube
self.set_parameter("ARSPD_RATIO", 0.1)
self.delay_sim_time(10)
if (self.get_parameter("ARSPD_USE") == 0):
self.progress("Faulty Sensor Disabled")
else:
raise NotAchievedException("Airspeed Sensor Not Disabled")
self.delay_sim_time(20)
# simulate the effect of blockage partially clearing
self.set_parameter("ARSPD_RATIO", 1.0)
self.delay_sim_time(60)
if (self.get_parameter("ARSPD_USE") == 0):
self.progress("Faulty Sensor Remains Disabled")
else:
raise NotAchievedException("Fault Sensor Re-Enabled")
# simulate the effect of blockage fully clearing
self.set_parameter("ARSPD_RATIO", 2.0)
self.delay_sim_time(60)
if (self.get_parameter("ARSPD_USE") == 1):
self.progress("Sensor Re-Enabled")
else:
raise NotAchievedException("Airspeed Sensor Not Re-Enabled")
self.fly_home_land_and_disarm()
def AIRSPEED_AUTOCAL(self):
'''Test AIRSPEED_AUTOCAL'''
self.progress("Ensure no AIRSPEED_AUTOCAL on ground")
self.set_parameters({
"ARSPD_AUTOCAL": 1,
"ARSPD_PIN": 2,
"ARSPD_RATIO": 0,
"ARSPD2_RATIO": 4,
"ARSPD2_TYPE": 3, # MS5525
"ARSPD2_BUS": 1,
"ARSPD2_AUTOCAL": 1,
"SIM_ARSPD2_OFS": 1900, # default is 2013
"RTL_AUTOLAND": 1,
})
self.context_collect('STATUSTEXT')
self.reboot_sitl()
self.assert_not_receive_message('AIRSPEED_AUTOCAL', timeout=5)
# these are boot-time calibration messages:
self.wait_statustext('Airspeed 1 calibrated', check_context=True, timeout=30)
self.wait_statustext('Airspeed 2 calibrated', check_context=True)
mission_filepath = "flaps.txt"
self.load_mission(mission_filepath)
self.wait_ready_to_arm()
self.arm_vehicle()
self.change_mode("AUTO")
self.progress("Ensure AIRSPEED_AUTOCAL in air")
self.assert_receive_message('AIRSPEED_AUTOCAL')
self.wait_statustext("Airspeed 0 ratio reset", check_context=True, timeout=70)
self.wait_statustext("Airspeed 1 ratio reset", check_context=True, timeout=70)
self.fly_home_land_and_disarm()
def deadreckoning_main(self, disable_airspeed_sensor=False):
self.reboot_sitl()
self.wait_ready_to_arm()
self.gpi = None
self.simstate = None
self.last_print = 0
self.max_divergence = 0
def validate_global_position_int_against_simstate(mav, m):
if m.get_type() == 'GLOBAL_POSITION_INT':
self.gpi = m
elif m.get_type() == 'SIMSTATE':
self.simstate = m
if self.gpi is None:
return
if self.simstate is None:
return
divergence = self.get_distance_int(self.gpi, self.simstate)
max_allowed_divergence = 200
if (time.time() - self.last_print > 1 or
divergence > self.max_divergence):
self.progress("position-estimate-divergence=%fm" % (divergence,))
self.last_print = time.time()
if divergence > self.max_divergence:
self.max_divergence = divergence
if divergence > max_allowed_divergence:
raise NotAchievedException(
"global-position-int diverged from simstate by %fm (max=%fm" %
(divergence, max_allowed_divergence,))
self.install_message_hook(validate_global_position_int_against_simstate)
try:
# wind is from the West:
self.set_parameter("SIM_WIND_DIR", 270)
# light winds:
self.set_parameter("SIM_WIND_SPD", 10)
if disable_airspeed_sensor:
self.set_parameter("ARSPD_USE", 0)
self.takeoff(50)
loc = self.mav.location()
self.location_offset_ne(loc, 500, 500)
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
p1=0,
p2=mavutil.mavlink.MAV_DO_REPOSITION_FLAGS_CHANGE_MODE,
p5=int(loc.lat * 1e7),
p6=int(loc.lng * 1e7),
p7=100, # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT_INT,
)
self.wait_location(loc, accuracy=100)
self.progress("Stewing")
self.delay_sim_time(20)
self.set_parameter("SIM_GPS_DISABLE", 1)
self.progress("Roasting")
self.delay_sim_time(20)
self.change_mode("RTL")
self.wait_distance_to_home(100, 200, timeout=200)
# go into LOITER to create additonal time for a GPS re-enable test
self.change_mode("LOITER")
self.set_parameter("SIM_GPS_DISABLE", 0)
t_enabled = self.get_sim_time()
# The EKF should wait for GPS checks to pass when we are still able to navigate using dead reckoning
# to prevent bad GPS being used when coming back after loss of lock due to interence.
self.wait_ekf_flags(mavutil.mavlink.ESTIMATOR_POS_HORIZ_ABS, 0, timeout=15)
if self.get_sim_time() < (t_enabled+9):
raise NotAchievedException("GPS use re-started too quickly")
# wait for EKF and vehicle position to stabilise, then test response to jamming
self.delay_sim_time(20)
self.set_parameter("AHRS_OPTIONS", 1)
self.set_parameter("SIM_GPS_JAM", 1)
self.delay_sim_time(10)
self.set_parameter("SIM_GPS_JAM", 0)
t_enabled = self.get_sim_time()
# The EKF should wait for GPS checks to pass when we are still able to navigate using dead reckoning
# to prevent bad GPS being used when coming back after loss of lock due to interence.
self.wait_ekf_flags(mavutil.mavlink.ESTIMATOR_POS_HORIZ_ABS, 0, timeout=15)
if self.get_sim_time() < (t_enabled+9):
raise NotAchievedException("GPS use re-started too quickly after jamming")
self.set_rc(3, 1000)
self.fly_home_land_and_disarm()
self.progress("max-divergence: %fm" % (self.max_divergence,))
finally:
self.remove_message_hook(validate_global_position_int_against_simstate)
def Deadreckoning(self):
'''Test deadreckoning support'''
self.deadreckoning_main()
def DeadreckoningNoAirSpeed(self):
'''Test deadreckoning support with no airspeed sensor'''
self.deadreckoning_main(disable_airspeed_sensor=True)
def ClimbBeforeTurn(self):
'''Test climb-before-turn'''
self.wait_ready_to_arm()
self.set_parameters({
"FLIGHT_OPTIONS": 0,
"RTL_ALTITUDE": 80,
"RTL_AUTOLAND": 1,
})
takeoff_alt = 10
self.takeoff(alt=takeoff_alt)
self.change_mode("CRUISE")
self.wait_distance_to_home(500, 1000, timeout=60)
self.change_mode("RTL")
expected_alt = self.get_parameter("RTL_ALTITUDE")
home = self.home_position_as_mav_location()
distance = self.get_distance(home, self.mav.location())
self.wait_altitude(expected_alt - 10, expected_alt + 10, relative=True, timeout=80)
new_distance = self.get_distance(home, self.mav.location())
# We should be closer to home.
if new_distance > distance:
raise NotAchievedException(
"Expected to be closer to home (was %fm, now %fm)."
% (distance, new_distance)
)
self.fly_home_land_and_disarm()
self.set_current_waypoint(0, check_afterwards=False)
self.change_mode("MANUAL")
self.set_rc(3, 1000)
self.wait_ready_to_arm()
self.set_parameters({
"FLIGHT_OPTIONS": 16,
"RTL_ALTITUDE": 100,
})
self.takeoff(alt=takeoff_alt)
self.change_mode("CRUISE")
self.wait_distance_to_home(500, 1000, timeout=60)
self.change_mode("RTL")
home = self.home_position_as_mav_location()
distance = self.get_distance(home, self.mav.location())
self.wait_altitude(expected_alt - 10, expected_alt + 10, relative=True, timeout=80)
new_distance = self.get_distance(home, self.mav.location())
# We should be farther from to home.
if new_distance < distance:
raise NotAchievedException(
"Expected to be farther from home (was %fm, now %fm)."
% (distance, new_distance)
)
self.fly_home_land_and_disarm(timeout=240)
def RTL_CLIMB_MIN(self):
'''Test RTL_CLIMB_MIN'''
self.wait_ready_to_arm()
rtl_climb_min = 100
self.set_parameter("RTL_CLIMB_MIN", rtl_climb_min)
takeoff_alt = 50
self.takeoff(alt=takeoff_alt)
self.change_mode('CRUISE')
self.wait_distance_to_home(1000, 1500, timeout=60)
post_cruise_alt = self.get_altitude(relative=True)
self.change_mode('RTL')
expected_alt = self.get_parameter("RTL_ALTITUDE")
if expected_alt == -1:
expected_alt = self.get_altitude(relative=True)
# ensure we're about half-way-down at the half-way-home stage:
self.wait_distance_to_nav_target(
0,
500,
timeout=240,
)
alt = self.get_altitude(relative=True)
expected_halfway_alt = expected_alt + (post_cruise_alt + rtl_climb_min - expected_alt)/2.0
if abs(alt - expected_halfway_alt) > 30:
raise NotAchievedException("Not half-way-down and half-way-home (want=%f got=%f" %
(expected_halfway_alt, alt))
self.progress("Half-way-down at half-way-home (want=%f vs got=%f)" %
(expected_halfway_alt, alt))
rtl_radius = self.get_parameter("RTL_RADIUS")
if rtl_radius == 0:
rtl_radius = self.get_parameter("WP_LOITER_RAD")
self.wait_distance_to_nav_target(
0,
rtl_radius,
timeout=120,
)
alt = self.get_altitude(relative=True)
if abs(alt - expected_alt) > 10:
raise NotAchievedException(
"Expected to have %fm altitude at end of RTL (got %f)" %
(expected_alt, alt))
self.fly_home_land_and_disarm()
def sample_enable_parameter(self):
return "Q_ENABLE"
def RangeFinder(self):
'''Test RangeFinder Basic Functionality'''
self.context_push()
self.progress("Making sure we don't ordinarily get RANGEFINDER")
self.assert_not_receive_message('RANGEFDINDER')
self.set_analog_rangefinder_parameters()
self.reboot_sitl()
'''ensure rangefinder gives height-above-ground'''
self.load_mission("plane-gripper-mission.txt") # borrow this
self.set_parameter("RTL_AUTOLAND", 1)
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_waypoint(5, 5, max_dist=100)
rf = self.mav.recv_match(type="RANGEFINDER", timeout=1, blocking=True)
if rf is None:
raise NotAchievedException("Did not receive rangefinder message")
gpi = self.mav.recv_match(type='GLOBAL_POSITION_INT', blocking=True, timeout=1)
if gpi is None:
raise NotAchievedException("Did not receive GLOBAL_POSITION_INT message")
if abs(rf.distance - gpi.relative_alt/1000.0) > 3:
raise NotAchievedException(
"rangefinder alt (%s) disagrees with global-position-int.relative_alt (%s)" %
(rf.distance, gpi.relative_alt/1000.0))
self.wait_statustext("Auto disarmed", timeout=60)
self.progress("Ensure RFND messages in log")
if not self.current_onboard_log_contains_message("RFND"):
raise NotAchievedException("No RFND messages in log")
self.context_pop()
self.reboot_sitl()
def rc_defaults(self):
ret = super(AutoTestPlane, self).rc_defaults()
ret[3] = 1000
ret[8] = 1800
return ret
def initial_mode_switch_mode(self):
return "MANUAL"
def default_mode(self):
return "MANUAL"
def PIDTuning(self):
'''Test PID Tuning'''
self.change_mode("FBWA") # we don't update PIDs in MANUAL
super(AutoTestPlane, self).PIDTuning()
def AuxModeSwitch(self):
'''Set modes via auxswitches'''
self.set_parameter("FLTMODE1", 1) # circle
self.set_rc(8, 950)
self.wait_mode("CIRCLE")
self.set_rc(9, 1000)
self.set_rc(10, 1000)
self.set_parameters({
"RC9_OPTION": 4, # RTL
"RC10_OPTION": 55, # guided
})
self.set_rc(9, 1900)
self.wait_mode("RTL")
self.set_rc(10, 1900)
self.wait_mode("GUIDED")
self.progress("resetting both switches - should go back to CIRCLE")
self.set_rc(9, 1000)
self.set_rc(10, 1000)
self.wait_mode("CIRCLE")
self.set_rc(9, 1900)
self.wait_mode("RTL")
self.set_rc(10, 1900)
self.wait_mode("GUIDED")
self.progress("Resetting switch should repoll mode switch")
self.set_rc(10, 1000) # this re-polls the mode switch
self.wait_mode("CIRCLE")
self.set_rc(9, 1000)
def wait_for_collision_threat_to_clear(self):
'''wait to get a "clear" collision message", then slurp remaining
messages'''
last_collision = self.get_sim_time()
while True:
now = self.get_sim_time()
if now - last_collision > 5:
return
self.progress("Waiting for collision message")
m = self.mav.recv_match(type='COLLISION', blocking=True, timeout=1)
self.progress("Got (%s)" % str(m))
if m is None:
continue
last_collision = now
def SimADSB(self):
'''Tests to ensure simulated ADSB sensor continues to function'''
self.set_parameters({
"SIM_ADSB_COUNT": 1,
"ADSB_TYPE": 1,
})
self.reboot_sitl()
self.assert_receive_message('ADSB_VEHICLE', timeout=30)
def ADSB(self):
'''Test ADSB'''
self.ADSB_f_action_rtl()
self.ADSB_r_action_resume_or_loiter()
def ADSB_r_action_resume_or_loiter(self):
'''ensure we resume auto mission or enter loiter'''
self.set_parameters({
"ADSB_TYPE": 1,
"AVD_ENABLE": 1,
"AVD_F_ACTION": mavutil.mavlink.MAV_COLLISION_ACTION_MOVE_HORIZONTALLY,
"AVD_F_RCVRY": 3, # resume auto or loiter
})
self.reboot_sitl()
self.takeoff(50)
# fly North, create thread to east, wait for flying east
self.start_subtest("Testing loiter resume")
self.reach_heading_manual(0)
here = self.mav.location()
self.test_adsb_send_threatening_adsb_message(here, offset_ne=(0, 30))
self.wait_mode('AVOID_ADSB')
# recovery has the vehicle circling a point... but we don't
# know which point. So wait 'til it looks like it is
# circling, then grab the point, then check we're circling
# it...
self.wait_heading(290)
self.wait_heading(300)
dest = self.position_target_loc()
REALLY_BAD_FUDGE_FACTOR = 1.25 # FIXME
expected_radius = REALLY_BAD_FUDGE_FACTOR * self.get_parameter('WP_LOITER_RAD')
self.wait_circling_point_with_radius(dest, expected_radius)
self.start_subtest("Testing mission resume")
self.reach_heading_manual(270)
self.load_generic_mission("CMAC-circuit.txt", strict=False)
self.change_mode('AUTO')
self.wait_current_waypoint(2)
self.test_adsb_send_threatening_adsb_message(here, offset_ne=(0, 30))
self.wait_mode('AVOID_ADSB')
self.wait_mode('AUTO')
self.fly_home_land_and_disarm()
def ADSB_f_action_rtl(self):
self.context_push()
ex = None
try:
# message ADSB_VEHICLE 37 -353632614 1491652305 0 584070 0 0 0 "bob" 3 1 255 17
self.set_parameter("RC12_OPTION", 38) # avoid-adsb
self.set_rc(12, 2000)
self.set_parameters({
"ADSB_TYPE": 1,
"AVD_ENABLE": 1,
"AVD_F_ACTION": mavutil.mavlink.MAV_COLLISION_ACTION_RTL,
})
self.reboot_sitl()
self.wait_ready_to_arm()
here = self.mav.location()
self.change_mode("FBWA")
self.delay_sim_time(2) # TODO: work out why this is required...
self.test_adsb_send_threatening_adsb_message(here)
self.progress("Waiting for collision message")
m = self.assert_receive_message('COLLISION', timeout=4)
if m.threat_level != 2:
raise NotAchievedException("Expected some threat at least")
if m.action != mavutil.mavlink.MAV_COLLISION_ACTION_RTL:
raise NotAchievedException("Incorrect action; want=%u got=%u" %
(mavutil.mavlink.MAV_COLLISION_ACTION_RTL, m.action))
self.wait_mode("RTL")
self.progress("Sending far-away ABSD_VEHICLE message")
self.mav.mav.adsb_vehicle_send(
37, # ICAO address
int(here.lat+1 * 1e7),
int(here.lng * 1e7),
mavutil.mavlink.ADSB_ALTITUDE_TYPE_PRESSURE_QNH,
int(here.alt*1000 + 10000), # 10m up
0, # heading in cdeg
0, # horizontal velocity cm/s
0, # vertical velocity cm/s
"bob".encode("ascii"), # callsign
mavutil.mavlink.ADSB_EMITTER_TYPE_LIGHT,
1, # time since last communication
65535, # flags
17 # squawk
)
self.wait_for_collision_threat_to_clear()
self.change_mode("FBWA")
self.progress("Disabling ADSB-avoidance with RC channel")
self.set_rc(12, 1000)
self.delay_sim_time(1) # let the switch get polled
self.test_adsb_send_threatening_adsb_message(here)
m = self.mav.recv_match(type='COLLISION', blocking=True, timeout=4)
self.progress("Got (%s)" % str(m))
if m is not None:
raise NotAchievedException("Got collision message when I shouldn't have")
except Exception as e:
self.print_exception_caught(e)
ex = e
self.context_pop()
self.reboot_sitl()
if ex is not None:
raise ex
def GuidedRequest(self, target_system=1, target_component=1):
'''Test handling of MISSION_ITEM in guided mode'''
self.progress("Takeoff")
self.takeoff(alt=50)
self.set_rc(3, 1500)
self.start_subtest("Ensure command bounced outside guided mode")
desired_relative_alt = 33
loc = self.mav.location()
self.location_offset_ne(loc, 300, 300)
loc.alt += desired_relative_alt
self.mav.mav.mission_item_int_send(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_NAV_WAYPOINT,
2, # current - guided-mode request
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
int(loc.lat * 1e7), # latitude
int(loc.lng * 1e7), # longitude
loc.alt, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
m = self.assert_receive_message('MISSION_ACK', timeout=5)
if m.type != mavutil.mavlink.MAV_MISSION_ERROR:
raise NotAchievedException("Did not get appropriate error")
self.start_subtest("Enter guided and flying somewhere constant")
self.change_mode("GUIDED")
self.mav.mav.mission_item_int_send(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT,
mavutil.mavlink.MAV_CMD_NAV_WAYPOINT,
2, # current - guided-mode request
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
int(loc.lat * 1e7), # latitude
int(loc.lng * 1e7), # longitude
desired_relative_alt, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
m = self.assert_receive_message('MISSION_ACK', timeout=5)
if m.type != mavutil.mavlink.MAV_MISSION_ACCEPTED:
raise NotAchievedException("Did not get accepted response")
self.wait_location(loc, accuracy=100) # based on loiter radius
self.wait_altitude(altitude_min=desired_relative_alt-3,
altitude_max=desired_relative_alt+3,
relative=True,
timeout=30)
self.start_subtest("changing alt with mission item in guided mode")
# test changing alt only - NOTE - this is still a
# NAV_WAYPOINT, not a changel-alt request!
desired_relative_alt = desired_relative_alt + 50
self.mav.mav.mission_item_int_send(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT,
mavutil.mavlink.MAV_CMD_NAV_WAYPOINT,
3, # current - change-alt request
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0,
desired_relative_alt, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
self.wait_altitude(altitude_min=desired_relative_alt-3,
altitude_max=desired_relative_alt+3,
relative=True,
timeout=30)
self.fly_home_land_and_disarm()
def LOITER(self):
'''Test Loiter mode'''
# first test old loiter behavour
self.set_parameter("FLIGHT_OPTIONS", 0)
self.takeoff(alt=200)
self.set_rc(3, 1500)
self.change_mode("LOITER")
self.progress("Doing a bit of loitering to start with")
tstart = self.get_sim_time()
while True:
now = self.get_sim_time_cached()
if now - tstart > 60:
break
m = self.mav.recv_match(type='VFR_HUD', blocking=True, timeout=5)
if m is None:
raise NotAchievedException("Did not get VFR_HUD")
new_throttle = m.throttle
alt = m.alt
m = self.assert_receive_message('ATTITUDE', timeout=5)
pitch = math.degrees(m.pitch)
self.progress("Pitch:%f throttle:%u alt:%f" % (pitch, new_throttle, alt))
m = self.assert_receive_message('VFR_HUD', timeout=5)
initial_throttle = m.throttle
initial_alt = m.alt
self.progress("Initial throttle: %u" % initial_throttle)
# pitch down, ensure throttle decreases:
rc2_max = self.get_parameter("RC2_MAX")
self.set_rc(2, int(rc2_max))
tstart = self.get_sim_time()
while True:
now = self.get_sim_time_cached()
'''stick-mixing is pushing the aircraft down. It doesn't want to go
down (the target loiter altitude hasn't changed), so it
tries to add energy by increasing the throttle.
'''
if now - tstart > 60:
raise NotAchievedException("Did not see increase in throttle")
m = self.assert_receive_message('VFR_HUD', timeout=5)
new_throttle = m.throttle
alt = m.alt
m = self.assert_receive_message('ATTITUDE', timeout=5)
pitch = math.degrees(m.pitch)
self.progress("Pitch:%f throttle:%u alt:%f" % (pitch, new_throttle, alt))
if new_throttle - initial_throttle > 20:
self.progress("Throttle delta achieved")
break
self.progress("Centering elevator and ensuring we get back to loiter altitude")
self.set_rc(2, 1500)
self.wait_altitude(initial_alt-1, initial_alt+1)
# Test new loiter behavour
self.set_parameter("FLIGHT_OPTIONS", 1 << 12)
# should decend at max stick
self.set_rc(2, int(rc2_max))
self.wait_altitude(initial_alt - 110, initial_alt - 90, timeout=90)
# should not climb back at mid stick
self.set_rc(2, 1500)
self.delay_sim_time(60)
self.wait_altitude(initial_alt - 110, initial_alt - 90)
# should climb at min stick
self.set_rc(2, 1100)
self.wait_altitude(initial_alt - 10, initial_alt + 10, timeout=90)
# return stick to center and fly home
self.set_rc(2, 1500)
self.fly_home_land_and_disarm()
def CPUFailsafe(self):
'''In lockup Plane should copy RC inputs to RC outputs'''
self.plane_CPUFailsafe()
def LargeMissions(self):
'''Test Manipulation of Large missions'''
self.load_mission("Kingaroy-vlarge.txt", strict=False)
self.load_mission("Kingaroy-vlarge2.txt", strict=False)
def Soaring(self):
'''Test Soaring feature'''
model = "plane-soaring"
self.customise_SITL_commandline(
[],
model=model,
defaults_filepath=self.model_defaults_filepath(model),
wipe=True)
self.load_mission('CMAC-soar.txt', strict=False)
# Enable thermalling RC
rc_chan = 0
for i in range(8):
rcx_option = self.get_parameter('RC{0}_OPTION'.format(i+1))
if rcx_option == 88:
rc_chan = i+1
break
if rc_chan == 0:
raise NotAchievedException("Did not find soaring enable channel option.")
self.set_rc_from_map({
rc_chan: 1900,
})
self.set_parameters({
"SOAR_VSPEED": 0.55,
"SOAR_MIN_THML_S": 25,
})
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
# Wait to detect thermal
self.progress("Waiting for thermal")
self.wait_mode('THERMAL', timeout=600)
# Wait to climb to SOAR_ALT_MAX
self.progress("Waiting for climb to max altitude")
alt_max = self.get_parameter('SOAR_ALT_MAX')
self.wait_altitude(alt_max-10, alt_max, timeout=600, relative=True)
# Wait for AUTO
self.progress("Waiting for AUTO mode")
self.wait_mode('AUTO')
# Disable thermals
self.set_parameter("SIM_THML_SCENARI", 0)
# Wait to descend to SOAR_ALT_MIN
self.progress("Waiting for glide to min altitude")
alt_min = self.get_parameter('SOAR_ALT_MIN')
self.wait_altitude(alt_min-10, alt_min, timeout=600, relative=True)
self.progress("Waiting for throttle up")
self.wait_servo_channel_value(3, 1200, timeout=5, comparator=operator.gt)
self.progress("Waiting for climb to cutoff altitude")
alt_ctf = self.get_parameter('SOAR_ALT_CUTOFF')
self.wait_altitude(alt_ctf-10, alt_ctf, timeout=600, relative=True)
# Allow time to suppress throttle and start descent.
self.delay_sim_time(20)
# Now set FBWB mode
self.change_mode('FBWB')
self.delay_sim_time(5)
# Now disable soaring (should hold altitude)
self.set_parameter("SOAR_ENABLE", 0)
self.delay_sim_time(10)
# And reenable. This should force throttle-down
self.set_parameter("SOAR_ENABLE", 1)
self.delay_sim_time(10)
# Now wait for descent and check throttle up
self.wait_altitude(alt_min-10, alt_min, timeout=600, relative=True)
self.progress("Waiting for climb")
self.wait_altitude(alt_ctf-10, alt_ctf, timeout=600, relative=True)
# Back to auto
self.change_mode('AUTO')
# Reenable thermals
self.set_parameter("SIM_THML_SCENARI", 1)
# Disable soaring using RC channel.
self.set_rc(rc_chan, 1100)
# Wait to get back to waypoint before thermal.
self.progress("Waiting to get back to position")
self.wait_current_waypoint(3, timeout=1200)
# Enable soaring with mode changes suppressed)
self.set_rc(rc_chan, 1500)
# Make sure this causes throttle down.
self.wait_servo_channel_value(3, 1200, timeout=3, comparator=operator.lt)
self.progress("Waiting for next WP with no thermalling")
self.wait_waypoint(4, 4, timeout=1200, max_dist=120)
# Disarm
self.disarm_vehicle_expect_fail()
self.progress("Mission OK")
def SpeedToFly(self):
'''Test soaring speed-to-fly'''
model = "plane-soaring"
self.customise_SITL_commandline(
[],
model=model,
defaults_filepath=self.model_defaults_filepath(model),
wipe=True)
self.load_mission('CMAC-soar.txt', strict=False)
self.set_parameters({
"SIM_THML_SCENARI": 0, # Turn off environmental thermals.
"SOAR_ALT_MAX": 1000, # remove source of random failure
})
# Get thermalling RC channel
rc_chan = 0
for i in range(8):
rcx_option = self.get_parameter('RC{0}_OPTION'.format(i+1))
if rcx_option == 88:
rc_chan = i+1
break
if rc_chan == 0:
raise NotAchievedException("Did not find soaring enable channel option.")
# Disable soaring
self.set_rc(rc_chan, 1100)
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
# Wait for to 400m before starting.
self.wait_altitude(390, 400, timeout=600, relative=True)
# Wait 10s to stabilize.
self.delay_sim_time(30)
# Enable soaring (no automatic thermalling)
self.set_rc(rc_chan, 1500)
self.set_parameters({
"SOAR_CRSE_ARSPD": -1, # Enable speed to fly.
"SOAR_VSPEED": 1, # Set appropriate McCready.
"SIM_WIND_SPD": 0,
})
self.progress('Waiting a few seconds before determining the "trim" airspeed.')
self.delay_sim_time(20)
m = self.assert_receive_message('VFR_HUD')
trim_airspeed = m.airspeed
self.progress("Using trim_airspeed=%f" % (trim_airspeed,))
min_airspeed = self.get_parameter("AIRSPEED_MIN")
max_airspeed = self.get_parameter("AIRSPEED_MAX")
if trim_airspeed > max_airspeed:
raise NotAchievedException("trim airspeed > max_airspeed (%f>%f)" %
(trim_airspeed, max_airspeed))
if trim_airspeed < min_airspeed:
raise NotAchievedException("trim airspeed < min_airspeed (%f<%f)" %
(trim_airspeed, min_airspeed))
self.progress("Adding updraft")
self.set_parameters({
"SIM_WIND_SPD": 1,
'SIM_WIND_DIR_Z': 90,
})
self.progress("Waiting for vehicle to move slower in updraft")
self.wait_airspeed(0, trim_airspeed-0.5, minimum_duration=10, timeout=120)
self.progress("Adding downdraft")
self.set_parameter('SIM_WIND_DIR_Z', -90)
self.progress("Waiting for vehicle to move faster in downdraft")
self.wait_airspeed(trim_airspeed+0.5, trim_airspeed+100, minimum_duration=10, timeout=120)
self.progress("Zeroing wind and increasing McCready")
self.set_parameters({
"SIM_WIND_SPD": 0,
"SOAR_VSPEED": 2,
})
self.progress("Waiting for airspeed to increase with higher VSPEED")
self.wait_airspeed(trim_airspeed+0.5, trim_airspeed+100, minimum_duration=10, timeout=120)
# mcReady tests don't work ATM, so just return early:
# takes too long to land, so just make it all go away:
self.disarm_vehicle(force=True)
self.reboot_sitl()
return
self.start_subtest('Test McReady values')
# Disable soaring
self.set_rc(rc_chan, 1100)
# Wait for to 400m before starting.
self.wait_altitude(390, 400, timeout=600, relative=True)
# Enable soaring
self.set_rc(rc_chan, 2000)
self.progress("Find airspeed with 1m/s updraft and mcready=1")
self.set_parameters({
"SOAR_VSPEED": 1,
"SIM_WIND_SPD": 1,
})
self.delay_sim_time(20)
m = self.assert_receive_message('VFR_HUD')
mcready1_speed = m.airspeed
self.progress("airspeed is %f" % mcready1_speed)
self.progress("Reducing McCready")
self.set_parameters({
"SOAR_VSPEED": 0.5,
})
self.progress("Waiting for airspeed to decrease with lower McReady")
self.wait_airspeed(0, mcready1_speed-0.5, minimum_duration=10, timeout=120)
self.progress("Increasing McCready")
self.set_parameters({
"SOAR_VSPEED": 1.5,
})
self.progress("Waiting for airspeed to decrease with lower McReady")
self.wait_airspeed(mcready1_speed+0.5, mcready1_speed+100, minimum_duration=10, timeout=120)
# takes too long to land, so just make it all go away:
self.disarm_vehicle(force=True)
self.reboot_sitl()
def AirspeedDrivers(self):
'''Test AirSpeed drivers'''
airspeed_sensors = [
("MS5525", 3, 1),
("DLVR", 7, 2),
("SITL", 100, 0),
]
for (name, t, bus) in airspeed_sensors:
self.context_push()
if bus is not None:
self.set_parameter("ARSPD2_BUS", bus)
self.set_parameter("ARSPD2_TYPE", t)
self.reboot_sitl()
self.wait_ready_to_arm()
self.arm_vehicle()
# insert listener to compare airspeeds:
airspeed = [None, None]
# don't start testing until we've seen real speed from
# both sensors. This gets us out of the noise area.
global initial_airspeed_threshold_reached
initial_airspeed_threshold_reached = False
def check_airspeeds(mav, m):
global initial_airspeed_threshold_reached
m_type = m.get_type()
if (m_type == 'NAMED_VALUE_FLOAT' and
m.name == 'AS2'):
airspeed[1] = m.value
elif m_type == 'VFR_HUD':
airspeed[0] = m.airspeed
else:
return
if airspeed[0] is None or airspeed[1] is None:
return
if airspeed[0] < 2 or airspeed[1] < 2:
# this mismatch can occur on takeoff, or when we
# smack into the ground at the end of the mission
return
if not initial_airspeed_threshold_reached:
if not (airspeed[0] > 10 or airspeed[1] > 10):
return
initial_airspeed_threshold_reached = True
delta = abs(airspeed[0] - airspeed[1])
if delta > 2:
raise NotAchievedException("Airspeed mismatch (as1=%f as2=%f)" % (airspeed[0], airspeed[1]))
self.install_message_hook_context(check_airspeeds)
self.fly_mission("ap1.txt", strict=False)
if airspeed[0] is None:
raise NotAchievedException("Never saw an airspeed1")
if airspeed[1] is None:
raise NotAchievedException("Never saw an airspeed2")
self.context_pop()
self.reboot_sitl()
def TerrainMission(self):
'''Test terrain following in mission'''
self.install_terrain_handlers_context()
num_wp = self.load_mission("ap-terrain.txt")
self.wait_ready_to_arm()
self.arm_vehicle()
global max_alt
max_alt = 0
def record_maxalt(mav, m):
global max_alt
if m.get_type() != 'GLOBAL_POSITION_INT':
return
if m.relative_alt/1000.0 > max_alt:
max_alt = m.relative_alt/1000.0
self.install_message_hook_context(record_maxalt)
self.fly_mission_waypoints(num_wp-1, mission_timeout=600)
if max_alt < 200:
raise NotAchievedException("Did not follow terrain")
def Terrain(self):
'''test AP_Terrain'''
self.reboot_sitl() # we know the terrain height at CMAC
self.install_terrain_handlers_context()
self.wait_ready_to_arm()
loc = self.mav.location()
lng_int = int(loc.lng * 1e7)
lat_int = int(loc.lat * 1e7)
# FIXME: once we have a pre-populated terrain cache this
# should require an instantly correct report to pass
tstart = self.get_sim_time_cached()
last_terrain_report_pending = -1
while True:
now = self.get_sim_time_cached()
if now - tstart > 60:
raise NotAchievedException("Did not get correct terrain report")
self.mav.mav.terrain_check_send(lat_int, lng_int)
report = self.mav.recv_match(type='TERRAIN_REPORT', blocking=True, timeout=60)
self.progress(self.dump_message_verbose(report))
if report.spacing != 0:
break
# we will keep trying to long as the number of pending
# tiles is dropping:
if last_terrain_report_pending == -1:
last_terrain_report_pending = report.pending
elif report.pending < last_terrain_report_pending:
last_terrain_report_pending = report.pending
tstart = now
self.delay_sim_time(1)
self.progress(self.dump_message_verbose(report))
expected_terrain_height = 583.5
if abs(report.terrain_height - expected_terrain_height) > 0.5:
raise NotAchievedException("Expected terrain height=%f got=%f" %
(expected_terrain_height, report.terrain_height))
def TerrainLoiter(self):
'''Test terrain following in loiter'''
self.context_push()
self.set_parameters({
"TERRAIN_FOLLOW": 1, # enable terrain following in loiter
"WP_LOITER_RAD": 2000, # set very large loiter rad to get some terrain changes
})
alt = 200
self.takeoff(alt*0.9, alt*1.1)
self.set_rc(3, 1500)
self.change_mode("LOITER")
self.progress("loitering at %um" % alt)
tstart = self.get_sim_time()
timeout = 60*15 # enough time to do one and a bit circles
max_delta = 0
while True:
now = self.get_sim_time_cached()
if now - tstart > timeout:
break
gpi = self.assert_receive_message('GLOBAL_POSITION_INT')
terrain = self.assert_receive_message('TERRAIN_REPORT')
rel_alt = terrain.current_height
self.progress("%um above terrain (%um bove home)" %
(rel_alt, gpi.relative_alt/1000.0))
if rel_alt > alt*1.2 or rel_alt < alt * 0.8:
raise NotAchievedException("Not terrain following")
delta = abs(rel_alt - gpi.relative_alt/1000.0)
if delta > max_delta:
max_delta = delta
want_max_delta = 30
if max_delta < want_max_delta:
raise NotAchievedException(
"Expected terrain and home alts to vary more than they did (max=%u want=%u)" %
(max_delta, want_max_delta))
self.context_pop()
self.progress("Returning home")
self.fly_home_land_and_disarm(240)
def fly_external_AHRS(self, sim, eahrs_type, mission):
"""Fly with external AHRS"""
self.customise_SITL_commandline(["--serial4=sim:%s" % sim])
self.set_parameters({
"EAHRS_TYPE": eahrs_type,
"SERIAL4_PROTOCOL": 36,
"SERIAL4_BAUD": 230400,
"GPS1_TYPE": 21,
"AHRS_EKF_TYPE": 11,
"INS_GYR_CAL": 1,
})
self.reboot_sitl()
self.delay_sim_time(5)
self.progress("Running accelcal")
self.run_cmd(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=4,
timeout=5,
)
self.wait_ready_to_arm()
self.arm_vehicle()
self.fly_mission(mission)
def wait_and_maintain_wind_estimate(
self,
want_speed,
want_dir,
timeout=10,
speed_tolerance=0.5,
dir_tolerance=5,
**kwargs):
'''wait for wind estimate to reach speed and direction'''
def validator(last, _min, _max):
'''returns false of spd or direction is too-far wrong'''
(spd, di) = last
_min_spd, _min_dir = _min
_max_spd, _max_dir = _max
if spd < _min_spd or spd > _max_spd:
return False
# my apologies to whoever is staring at this and wondering
# why we're not wrapping angles here...
if di < _min_dir or di > _max_dir:
return False
return True
def value_getter():
'''returns a tuple of (wind_speed, wind_dir), where wind_dir is 45 if
wind is coming from NE'''
m = self.assert_receive_message("WIND")
return (m.speed, m.direction)
class ValueAverager(object):
def __init__(self):
self.speed_average = -1
self.dir_average = -1
self.count = 0.0
def add_value(self, value):
(spd, di) = value
if self.speed_average == -1:
self.speed_average = spd
self.dir_average = di
else:
self.speed_average += spd
self.di_average += spd
self.count += 1
return (self.speed_average/self.count, self.dir_average/self.count)
def reset(self):
self.count = 0
self.speed_average = -1
self.dir_average = -1
self.wait_and_maintain_range(
value_name="WindEstimates",
minimum=(want_speed-speed_tolerance, want_dir-dir_tolerance),
maximum=(want_speed+speed_tolerance, want_dir+dir_tolerance),
current_value_getter=value_getter,
value_averager=ValueAverager(),
validator=lambda last, _min, _max: validator(last, _min, _max),
timeout=timeout,
**kwargs
)
def WindEstimates(self):
'''fly non-external AHRS, ensure wind estimate correct'''
self.set_parameters({
"SIM_WIND_SPD": 5,
"SIM_WIND_DIR": 45,
})
self.wait_ready_to_arm()
self.takeoff(70) # default wind sim wind is a sqrt function up to 60m
self.change_mode('LOITER')
# use default estimator to determine when to check others:
self.wait_and_maintain_wind_estimate(5, 45, timeout=120)
for ahrs_type in 0, 2, 3, 10:
self.start_subtest("Checking AHRS_EKF_TYPE=%u" % ahrs_type)
self.set_parameter("AHRS_EKF_TYPE", ahrs_type)
self.wait_and_maintain_wind_estimate(
5, 45,
speed_tolerance=1,
timeout=30
)
self.fly_home_land_and_disarm()
def VectorNavEAHRS(self):
'''Test VectorNav EAHRS support'''
self.fly_external_AHRS("VectorNav", 1, "ap1.txt")
def MicroStrainEAHRS5(self):
'''Test MicroStrain EAHRS series 5 support'''
self.fly_external_AHRS("MicroStrain5", 2, "ap1.txt")
def MicroStrainEAHRS7(self):
'''Test MicroStrain EAHRS series 7 support'''
self.fly_external_AHRS("MicroStrain7", 7, "ap1.txt")
def InertialLabsEAHRS(self):
'''Test InertialLabs EAHRS support'''
self.fly_external_AHRS("ILabs", 5, "ap1.txt")
def GpsSensorPreArmEAHRS(self):
'''Test pre-arm checks related to EAHRS_SENSORS using the MicroStrain7 driver'''
self.customise_SITL_commandline(["--serial4=sim:MicroStrain7"])
self.set_parameters({
"EAHRS_TYPE": 7,
"SERIAL4_PROTOCOL": 36,
"SERIAL4_BAUD": 230400,
"GPS1_TYPE": 0, # Disabled (simulate user setup error)
"GPS2_TYPE": 0, # Disabled (simulate user setup error)
"AHRS_EKF_TYPE": 11,
"INS_GYR_CAL": 1,
"EAHRS_SENSORS": 13, # GPS is enabled
})
self.reboot_sitl()
self.delay_sim_time(5)
self.progress("Running accelcal")
self.run_cmd(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=4,
timeout=5,
)
self.assert_prearm_failure("ExternalAHRS: Incorrect number", # Cut short due to message limits.
timeout=30,
other_prearm_failures_fatal=False)
self.set_parameters({
"EAHRS_TYPE": 7,
"SERIAL4_PROTOCOL": 36,
"SERIAL4_BAUD": 230400,
"GPS1_TYPE": 1, # Auto
"GPS2_TYPE": 21, # EARHS
"AHRS_EKF_TYPE": 11,
"INS_GYR_CAL": 1,
"EAHRS_SENSORS": 13, # GPS is enabled
})
self.reboot_sitl()
self.delay_sim_time(5)
self.progress("Running accelcal")
self.run_cmd(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=4,
timeout=5,
)
# Check prearm success with MicroStrain when the first GPS is occupied by another GPS.
# This supports the use case of comparing MicroStrain dual antenna to another GPS.
self.wait_ready_to_arm()
def get_accelvec(self, m):
return Vector3(m.xacc, m.yacc, m.zacc) * 0.001 * 9.81
def get_gyrovec(self, m):
return Vector3(m.xgyro, m.ygyro, m.zgyro) * 0.001 * math.degrees(1)
def IMUTempCal(self):
'''Test IMU temperature calibration'''
self.progress("Setting up SITL temperature profile")
self.set_parameters({
"SIM_IMUT1_ENABLE" : 1,
"SIM_IMUT1_ACC1_X" : 120000.000000,
"SIM_IMUT1_ACC1_Y" : -190000.000000,
"SIM_IMUT1_ACC1_Z" : 1493.864746,
"SIM_IMUT1_ACC2_X" : -51.624416,
"SIM_IMUT1_ACC2_Y" : 10.364172,
"SIM_IMUT1_ACC2_Z" : -7878.000000,
"SIM_IMUT1_ACC3_X" : -0.514242,
"SIM_IMUT1_ACC3_Y" : 0.862218,
"SIM_IMUT1_ACC3_Z" : -234.000000,
"SIM_IMUT1_GYR1_X" : -5122.513817,
"SIM_IMUT1_GYR1_Y" : -3250.470428,
"SIM_IMUT1_GYR1_Z" : -2136.346676,
"SIM_IMUT1_GYR2_X" : 30.720505,
"SIM_IMUT1_GYR2_Y" : 17.778447,
"SIM_IMUT1_GYR2_Z" : 0.765997,
"SIM_IMUT1_GYR3_X" : -0.003572,
"SIM_IMUT1_GYR3_Y" : 0.036346,
"SIM_IMUT1_GYR3_Z" : 0.015457,
"SIM_IMUT1_TMAX" : 70.0,
"SIM_IMUT1_TMIN" : -20.000000,
"SIM_IMUT2_ENABLE" : 1,
"SIM_IMUT2_ACC1_X" : -160000.000000,
"SIM_IMUT2_ACC1_Y" : 198730.000000,
"SIM_IMUT2_ACC1_Z" : 27812.000000,
"SIM_IMUT2_ACC2_X" : 30.658159,
"SIM_IMUT2_ACC2_Y" : 32.085022,
"SIM_IMUT2_ACC2_Z" : 1572.000000,
"SIM_IMUT2_ACC3_X" : 0.102912,
"SIM_IMUT2_ACC3_Y" : 0.229734,
"SIM_IMUT2_ACC3_Z" : 172.000000,
"SIM_IMUT2_GYR1_X" : 3173.925644,
"SIM_IMUT2_GYR1_Y" : -2368.312836,
"SIM_IMUT2_GYR1_Z" : -1796.497177,
"SIM_IMUT2_GYR2_X" : 13.029696,
"SIM_IMUT2_GYR2_Y" : -10.349280,
"SIM_IMUT2_GYR2_Z" : -15.082653,
"SIM_IMUT2_GYR3_X" : 0.004831,
"SIM_IMUT2_GYR3_Y" : -0.020528,
"SIM_IMUT2_GYR3_Z" : 0.009469,
"SIM_IMUT2_TMAX" : 70.000000,
"SIM_IMUT2_TMIN" : -20.000000,
"SIM_IMUT_END" : 45.000000,
"SIM_IMUT_START" : 3.000000,
"SIM_IMUT_TCONST" : 75.000000,
"SIM_DRIFT_SPEED" : 0,
"INS_GYR_CAL" : 0,
})
self.set_parameter("SIM_IMUT_FIXED", 12)
self.progress("Running accel cal")
self.run_cmd(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=4,
timeout=5,
)
self.progress("Running gyro cal")
self.run_cmd(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=1,
timeout=5,
)
self.set_parameters({
"SIM_IMUT_FIXED": 0,
"INS_TCAL1_ENABLE": 2,
"INS_TCAL1_TMAX": 42,
"INS_TCAL2_ENABLE": 2,
"INS_TCAL2_TMAX": 42,
"SIM_SPEEDUP": 200,
})
self.set_parameter("LOG_DISARMED", 1)
self.reboot_sitl()
self.progress("Waiting for IMU temperature")
self.assert_reach_imu_temperature(43, timeout=600)
if self.get_parameter("INS_TCAL1_ENABLE") != 1.0:
raise NotAchievedException("TCAL1 did not complete")
if self.get_parameter("INS_TCAL2_ENABLE") != 1.0:
raise NotAchievedException("TCAL2 did not complete")
self.progress("Logging with calibration enabled")
self.reboot_sitl()
self.assert_reach_imu_temperature(43, timeout=600)
self.progress("Testing with compensation enabled")
test_temperatures = range(10, 45, 5)
corrected = {}
uncorrected = {}
for temp in test_temperatures:
self.progress("Testing temperature %.1f" % temp)
self.set_parameter("SIM_IMUT_FIXED", temp)
self.delay_sim_time(2)
for msg in ['RAW_IMU', 'SCALED_IMU2']:
m = self.assert_receive_message(msg, timeout=2)
temperature = m.temperature*0.01
if abs(temperature - temp) > 0.2:
raise NotAchievedException("incorrect %s temperature %.1f should be %.1f" % (msg, temperature, temp))
accel = self.get_accelvec(m)
gyro = self.get_gyrovec(m)
accel2 = accel + Vector3(0, 0, 9.81)
corrected[temperature] = (accel2, gyro)
self.progress("Testing with compensation disabled")
self.set_parameters({
"INS_TCAL1_ENABLE": 0,
"INS_TCAL2_ENABLE": 0,
})
gyro_threshold = 0.2
accel_threshold = 0.2
for temp in test_temperatures:
self.progress("Testing temperature %.1f" % temp)
self.set_parameter("SIM_IMUT_FIXED", temp)
self.wait_heartbeat()
self.wait_heartbeat()
for msg in ['RAW_IMU', 'SCALED_IMU2']:
m = self.assert_receive_message(msg, timeout=2)
temperature = m.temperature*0.01
if abs(temperature - temp) > 0.2:
raise NotAchievedException("incorrect %s temperature %.1f should be %.1f" % (msg, temperature, temp))
accel = self.get_accelvec(m)
gyro = self.get_gyrovec(m)
accel2 = accel + Vector3(0, 0, 9.81)
uncorrected[temperature] = (accel2, gyro)
for temp in test_temperatures:
(accel, gyro) = corrected[temp]
self.progress("Corrected gyro at %.1f %s" % (temp, gyro))
self.progress("Corrected accel at %.1f %s" % (temp, accel))
for temp in test_temperatures:
(accel, gyro) = uncorrected[temp]
self.progress("Uncorrected gyro at %.1f %s" % (temp, gyro))
self.progress("Uncorrected accel at %.1f %s" % (temp, accel))
bad_value = False
for temp in test_temperatures:
(accel, gyro) = corrected[temp]
if gyro.length() > gyro_threshold:
raise NotAchievedException("incorrect corrected at %.1f gyro %s" % (temp, gyro))
if accel.length() > accel_threshold:
raise NotAchievedException("incorrect corrected at %.1f accel %s" % (temp, accel))
(accel, gyro) = uncorrected[temp]
if gyro.length() > gyro_threshold*2:
bad_value = True
if accel.length() > accel_threshold*2:
bad_value = True
if not bad_value:
raise NotAchievedException("uncompensated IMUs did not vary enough")
# the above tests change the internal persistent state of the
# vehicle in ways that autotest doesn't track (magically set
# parameters). So wipe the vehicle's eeprom:
self.reset_SITL_commandline()
def EKFlaneswitch(self):
'''Test EKF3 Affinity and Lane Switching'''
self.context_push()
ex = None
# new lane swtich available only with EK3
self.set_parameters({
"EK3_ENABLE": 1,
"EK2_ENABLE": 0,
"AHRS_EKF_TYPE": 3,
"EK3_AFFINITY": 15, # enable affinity for all sensors
"EK3_IMU_MASK": 3, # use only 2 IMUs
"GPS2_TYPE": 1,
"SIM_GPS2_DISABLE": 0,
"SIM_BARO_COUNT": 2,
"SIM_BAR2_DISABLE": 0,
"ARSPD2_TYPE": 2,
"ARSPD2_USE": 1,
"ARSPD2_PIN": 2,
})
# some parameters need reboot to take effect
self.reboot_sitl()
self.lane_switches = []
# add an EKF lane switch hook
def statustext_hook(mav, message):
if message.get_type() != 'STATUSTEXT':
return
# example msg: EKF3 lane switch 1
if not message.text.startswith("EKF3 lane switch "):
return
newlane = int(message.text[-1])
self.lane_switches.append(newlane)
self.install_message_hook(statustext_hook)
# get flying
self.takeoff(alt=50)
self.change_mode('CIRCLE')
try:
###################################################################
self.progress("Checking EKF3 Lane Switching trigger from all sensors")
###################################################################
self.start_subtest("ACCELEROMETER: Change z-axis offset")
# create an accelerometer error by changing the Z-axis offset
self.context_collect("STATUSTEXT")
old_parameter = self.get_parameter("INS_ACCOFFS_Z")
self.wait_statustext(
text="EKF3 lane switch",
timeout=30,
the_function=self.set_parameter("INS_ACCOFFS_Z", old_parameter + 5),
check_context=True)
if self.lane_switches != [1]:
raise NotAchievedException("Expected lane switch 1, got %s" % str(self.lane_switches[-1]))
# Cleanup
self.set_parameter("INS_ACCOFFS_Z", old_parameter)
self.context_clear_collection("STATUSTEXT")
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
###################################################################
self.start_subtest("BAROMETER: Freeze to last measured value")
self.context_collect("STATUSTEXT")
# create a barometer error by inhibiting any pressure change while changing altitude
old_parameter = self.get_parameter("SIM_BAR2_FREEZE")
self.set_parameter("SIM_BAR2_FREEZE", 1)
self.wait_statustext(
text="EKF3 lane switch",
timeout=30,
the_function=lambda: self.set_rc(2, 2000),
check_context=True)
if self.lane_switches != [1, 0]:
raise NotAchievedException("Expected lane switch 0, got %s" % str(self.lane_switches[-1]))
# Cleanup
self.set_rc(2, 1500)
self.set_parameter("SIM_BAR2_FREEZE", old_parameter)
self.context_clear_collection("STATUSTEXT")
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
###################################################################
self.start_subtest("GPS: Apply GPS Velocity Error in NED")
self.context_push()
self.context_collect("STATUSTEXT")
# create a GPS velocity error by adding a random 2m/s
# noise on each axis
def sim_gps_verr():
self.set_parameters({
"SIM_GPS_VERR_X": self.get_parameter("SIM_GPS_VERR_X") + 2,
"SIM_GPS_VERR_Y": self.get_parameter("SIM_GPS_VERR_Y") + 2,
"SIM_GPS_VERR_Z": self.get_parameter("SIM_GPS_VERR_Z") + 2,
})
self.wait_statustext(text="EKF3 lane switch", timeout=30, the_function=sim_gps_verr, check_context=True)
if self.lane_switches != [1, 0, 1]:
raise NotAchievedException("Expected lane switch 1, got %s" % str(self.lane_switches[-1]))
# Cleanup
self.context_pop()
self.context_clear_collection("STATUSTEXT")
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
###################################################################
self.start_subtest("MAGNETOMETER: Change X-Axis Offset")
self.context_collect("STATUSTEXT")
# create a magnetometer error by changing the X-axis offset
old_parameter = self.get_parameter("SIM_MAG2_OFS_X")
self.wait_statustext(
text="EKF3 lane switch",
timeout=30,
the_function=self.set_parameter("SIM_MAG2_OFS_X", old_parameter + 150),
check_context=True)
if self.lane_switches != [1, 0, 1, 0]:
raise NotAchievedException("Expected lane switch 0, got %s" % str(self.lane_switches[-1]))
# Cleanup
self.set_parameter("SIM_MAG2_OFS_X", old_parameter)
self.context_clear_collection("STATUSTEXT")
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
###################################################################
self.start_subtest("AIRSPEED: Fail to constant value")
self.context_push()
self.context_collect("STATUSTEXT")
old_parameter = self.get_parameter("SIM_ARSPD_FAIL")
def fail_speed():
self.change_mode("GUIDED")
loc = self.mav.location()
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
p5=int(loc.lat * 1e7),
p6=int(loc.lng * 1e7),
p7=50, # alt
)
self.delay_sim_time(5)
# create an airspeed sensor error by freezing to the
# current airspeed then changing the airspeed demand
# to a higher value and waiting for the TECS speed
# loop to diverge
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
self.set_parameter("SIM_ARSPD_FAIL", m.airspeed)
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
p1=0, # airspeed
p2=30,
p3=-1, # throttle / no change
p4=0, # absolute values
)
self.wait_statustext(text="EKF3 lane switch", timeout=30, the_function=fail_speed, check_context=True)
if self.lane_switches != [1, 0, 1, 0, 1]:
raise NotAchievedException("Expected lane switch 1, got %s" % str(self.lane_switches[-1]))
# Cleanup
self.set_parameter("SIM_ARSPD_FAIL", old_parameter)
self.change_mode('CIRCLE')
self.context_pop()
self.context_clear_collection("STATUSTEXT")
self.wait_heading(0, accuracy=10, timeout=60)
self.wait_heading(180, accuracy=10, timeout=60)
###################################################################
self.progress("GYROSCOPE: Change Y-Axis Offset")
self.context_collect("STATUSTEXT")
# create a gyroscope error by changing the Y-axis offset
old_parameter = self.get_parameter("INS_GYR2OFFS_Y")
self.wait_statustext(
text="EKF3 lane switch",
timeout=30,
the_function=self.set_parameter("INS_GYR2OFFS_Y", old_parameter + 1),
check_context=True)
if self.lane_switches != [1, 0, 1, 0, 1, 0]:
raise NotAchievedException("Expected lane switch 0, got %s" % str(self.lane_switches[-1]))
# Cleanup
self.set_parameter("INS_GYR2OFFS_Y", old_parameter)
self.context_clear_collection("STATUSTEXT")
###################################################################
self.disarm_vehicle(force=True)
except Exception as e:
self.print_exception_caught(e)
ex = e
self.remove_message_hook(statustext_hook)
self.context_pop()
# some parameters need reboot to take effect
self.reboot_sitl()
if ex is not None:
raise ex
def FenceAltCeilFloor(self):
'''Tests the fence ceiling and floor'''
fence_bit = mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE
self.set_parameters({
"FENCE_TYPE": 9, # Set fence type to max and min alt
"FENCE_ACTION": 0, # Set action to report
"FENCE_ALT_MAX": 200,
"FENCE_ALT_MIN": 100,
})
# Grab Home Position
self.mav.recv_match(type='HOME_POSITION', blocking=True)
self.homeloc = self.mav.location()
cruise_alt = 150
self.takeoff(cruise_alt)
self.do_fence_enable()
self.progress("Fly above ceiling and check for breach")
self.change_altitude(self.homeloc.alt + cruise_alt + 80)
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
self.progress("Got (%s)" % str(m))
if ((m.onboard_control_sensors_health & fence_bit)):
raise NotAchievedException("Fence Ceiling did not breach")
self.progress("Return to cruise alt and check for breach clear")
self.change_altitude(self.homeloc.alt + cruise_alt)
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
self.progress("Got (%s)" % str(m))
if (not (m.onboard_control_sensors_health & fence_bit)):
raise NotAchievedException("Fence breach did not clear")
self.progress("Fly below floor and check for breach")
self.change_altitude(self.homeloc.alt + cruise_alt - 80)
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
self.progress("Got (%s)" % str(m))
if ((m.onboard_control_sensors_health & fence_bit)):
raise NotAchievedException("Fence Floor did not breach")
self.do_fence_disable()
self.fly_home_land_and_disarm(timeout=150)
def FenceBreachedChangeMode(self):
'''Tests manual mode change after fence breach, as set with FENCE_OPTIONS'''
""" Attempts to change mode while a fence is breached.
mode should change should fail if fence option bit is set"""
self.set_parameters({
"FENCE_ACTION": 1,
"FENCE_TYPE": 4,
})
home_loc = self.mav.location()
locs = [
mavutil.location(home_loc.lat - 0.001, home_loc.lng - 0.001, 0, 0),
mavutil.location(home_loc.lat - 0.001, home_loc.lng + 0.001, 0, 0),
mavutil.location(home_loc.lat + 0.001, home_loc.lng + 0.001, 0, 0),
mavutil.location(home_loc.lat + 0.001, home_loc.lng - 0.001, 0, 0),
]
self.upload_fences_from_locations(
mavutil.mavlink.MAV_CMD_NAV_FENCE_POLYGON_VERTEX_INCLUSION,
[
locs
]
)
self.delay_sim_time(1)
self.wait_ready_to_arm()
self.takeoff(alt=50)
self.change_mode("CRUISE")
self.wait_distance(250, accuracy=15)
self.progress("Enable fence and initiate fence action")
self.do_fence_enable()
self.assert_fence_enabled()
self.wait_mode("RTL") # We should RTL because of fence breach
self.progress("User mode change to cruise should retrigger fence action")
try:
# mode change should time out, 'WaitModeTimeout' exception is the desired resut
# cant wait too long or the vehicle will be inside fence and allow the mode change
self.change_mode("CRUISE", timeout=10)
raise NotAchievedException("Should not change mode in fence breach")
except WaitModeTimeout:
pass
except Exception as e:
raise e
# enable mode change
self.set_parameter("FENCE_OPTIONS", 0)
self.progress("Check user mode change to LOITER is allowed")
self.change_mode("LOITER")
# Fly for 20 seconds and make sure still in LOITER mode
self.delay_sim_time(20)
if not self.mode_is("LOITER"):
raise NotAchievedException("Fence should not re-trigger")
# reset options parameter
self.set_parameter("FENCE_OPTIONS", 1)
self.progress("Test complete, disable fence and come home")
self.do_fence_disable()
self.fly_home_land_and_disarm()
def FenceNoFenceReturnPoint(self):
'''Tests calculated return point during fence breach when no fence return point present'''
""" Attempts to change mode while a fence is breached.
This should revert to the mode specified by the fence action. """
want_radius = 100 # Fence Return Radius
self.set_parameters({
"FENCE_ACTION": 6,
"FENCE_TYPE": 4,
"RTL_RADIUS": want_radius,
"NAVL1_LIM_BANK": 60,
})
home_loc = self.mav.location()
locs = [
mavutil.location(home_loc.lat - 0.003, home_loc.lng - 0.001, 0, 0),
mavutil.location(home_loc.lat - 0.003, home_loc.lng + 0.003, 0, 0),
mavutil.location(home_loc.lat + 0.001, home_loc.lng + 0.003, 0, 0),
mavutil.location(home_loc.lat + 0.001, home_loc.lng - 0.001, 0, 0),
]
self.upload_fences_from_locations(
mavutil.mavlink.MAV_CMD_NAV_FENCE_POLYGON_VERTEX_INCLUSION,
[
locs
]
)
self.delay_sim_time(1)
self.wait_ready_to_arm()
self.takeoff(alt=50)
self.change_mode("CRUISE")
self.wait_distance(150, accuracy=20)
self.progress("Enable fence and initiate fence action")
self.do_fence_enable()
self.assert_fence_enabled()
self.wait_mode("GUIDED", timeout=120) # We should RTL because of fence breach
self.delay_sim_time(60)
items = self.download_using_mission_protocol(mavutil.mavlink.MAV_MISSION_TYPE_FENCE)
if len(items) != 4:
raise NotAchievedException("Unexpected fencepoint count (want=%u got=%u)" % (4, len(items)))
# Check there are no fence return points specified still
for fence_loc in items:
if fence_loc.command == mavutil.mavlink.MAV_CMD_NAV_FENCE_RETURN_POINT:
raise NotAchievedException(
"Unexpected fence return point found (%u) got %u" %
(fence_loc.command,
mavutil.mavlink.MAV_CMD_NAV_FENCE_RETURN_POINT))
# Work out the approximate return point when no fence return point present
# Logic taken from AC_PolyFence_loader.cpp
min_loc = self.mav.location()
max_loc = self.mav.location()
for new_loc in locs:
if new_loc.lat < min_loc.lat:
min_loc.lat = new_loc.lat
if new_loc.lng < min_loc.lng:
min_loc.lng = new_loc.lng
if new_loc.lat > max_loc.lat:
max_loc.lat = new_loc.lat
if new_loc.lng > max_loc.lng:
max_loc.lng = new_loc.lng
# Generate the return location based on min and max locs
ret_lat = (min_loc.lat + max_loc.lat) / 2
ret_lng = (min_loc.lng + max_loc.lng) / 2
ret_loc = mavutil.location(ret_lat, ret_lng, 0, 0)
self.progress("Return loc: (%s)" % str(ret_loc))
# Wait for guided return to vehicle calculated fence return location
self.wait_distance_to_location(ret_loc, 90, 110)
self.wait_circling_point_with_radius(ret_loc, 92)
self.progress("Test complete, disable fence and come home")
self.do_fence_disable()
self.fly_home_land_and_disarm()
def FenceNoFenceReturnPointInclusion(self):
'''Tests using home as fence return point when none is present, and no inclusion fence is uploaded'''
""" Test result when a breach occurs and No fence return point is present and
no inclusion fence is present and exclusion fence is present """
want_radius = 100 # Fence Return Radius
self.set_parameters({
"FENCE_ACTION": 6,
"FENCE_TYPE": 2,
"FENCE_RADIUS": 300,
"RTL_RADIUS": want_radius,
"NAVL1_LIM_BANK": 60,
})
self.clear_fence()
self.delay_sim_time(1)
self.wait_ready_to_arm()
home_loc = self.mav.location()
self.takeoff(alt=50)
self.change_mode("CRUISE")
self.wait_distance(150, accuracy=20)
self.progress("Enable fence and initiate fence action")
self.do_fence_enable()
self.assert_fence_enabled()
self.wait_mode("GUIDED") # We should RTL because of fence breach
self.delay_sim_time(30)
items = self.download_using_mission_protocol(mavutil.mavlink.MAV_MISSION_TYPE_FENCE)
if len(items) != 0:
raise NotAchievedException("Unexpected fencepoint count (want=%u got=%u)" % (0, len(items)))
# Check there are no fence return points specified still
for fence_loc in items:
if fence_loc.command == mavutil.mavlink.MAV_CMD_NAV_FENCE_RETURN_POINT:
raise NotAchievedException(
"Unexpected fence return point found (%u) got %u" %
(fence_loc.command,
mavutil.mavlink.MAV_CMD_NAV_FENCE_RETURN_POINT))
# Wait for guided return to vehicle calculated fence return location
self.wait_distance_to_location(home_loc, 90, 110)
self.wait_circling_point_with_radius(home_loc, 92)
self.progress("Test complete, disable fence and come home")
self.do_fence_disable()
self.fly_home_land_and_disarm()
def FenceDisableUnderAction(self):
'''Tests Disabling fence while undergoing action caused by breach'''
""" Fence breach will cause the vehicle to enter guided mode.
Upon breach clear, check the vehicle is in the expected mode"""
self.set_parameters({
"FENCE_ALT_MIN": 50, # Sets the fence floor
"FENCE_TYPE": 8, # Only use fence floor for breaches
})
self.wait_ready_to_arm()
def attempt_fence_breached_disable(start_mode, end_mode, expected_mode, action):
self.set_parameter("FENCE_ACTION", action) # Set Fence Action to Guided
self.change_mode(start_mode)
self.arm_vehicle()
self.do_fence_enable()
self.assert_fence_enabled()
self.wait_mode(expected_mode)
self.do_fence_disable()
self.assert_fence_disabled()
self.wait_mode(end_mode)
self.disarm_vehicle(force=True)
attempt_fence_breached_disable(start_mode="FBWA", end_mode="RTL", expected_mode="RTL", action=1)
attempt_fence_breached_disable(start_mode="FBWA", end_mode="FBWA", expected_mode="GUIDED", action=6)
attempt_fence_breached_disable(start_mode="FBWA", end_mode="FBWA", expected_mode="GUIDED", action=7)
def _MAV_CMD_DO_AUX_FUNCTION(self, run_cmd):
'''Test triggering Auxiliary Functions via mavlink'''
self.context_collect('STATUSTEXT')
self.run_auxfunc(64, 2, run_cmd=run_cmd) # 64 == reverse throttle
self.wait_statustext("RevThrottle: ENABLE", check_context=True)
self.run_auxfunc(64, 0, run_cmd=run_cmd)
self.wait_statustext("RevThrottle: DISABLE", check_context=True)
self.run_auxfunc(65, 2, run_cmd=run_cmd) # 65 == GPS_DISABLE
self.start_subtest("Bad auxfunc")
self.run_auxfunc(
65231,
2,
want_result=mavutil.mavlink.MAV_RESULT_FAILED,
run_cmd=run_cmd,
)
self.start_subtest("Bad switchpos")
self.run_auxfunc(
62,
17,
want_result=mavutil.mavlink.MAV_RESULT_DENIED,
run_cmd=run_cmd,
)
def MAV_CMD_DO_AUX_FUNCTION(self):
'''Test triggering Auxiliary Functions via mavlink'''
self._MAV_CMD_DO_AUX_FUNCTION(run_cmd=self.run_cmd)
self._MAV_CMD_DO_AUX_FUNCTION(run_cmd=self.run_cmd_int)
def FlyEachFrame(self):
'''Fly each supported internal frame'''
vinfo = vehicleinfo.VehicleInfo()
vinfo_options = vinfo.options[self.vehicleinfo_key()]
known_broken_frames = {
"plane-tailsitter": "does not take off; immediately emits 'AP: Transition VTOL done' while on ground",
"plane-ice" : "needs ICE control channel for ignition",
"quadplane-ice" : "needs ICE control channel for ignition",
"quadplane-can" : "needs CAN periph",
"stratoblimp" : "not expected to fly normally",
"glider" : "needs balloon lift",
}
for frame in sorted(vinfo_options["frames"].keys()):
self.start_subtest("Testing frame (%s)" % str(frame))
if frame in known_broken_frames:
self.progress("Actually, no I'm not - it is known-broken (%s)" %
(known_broken_frames[frame]))
continue
frame_bits = vinfo_options["frames"][frame]
print("frame_bits: %s" % str(frame_bits))
if frame_bits.get("external", False):
self.progress("Actually, no I'm not - it is an external simulation")
continue
model = frame_bits.get("model", frame)
# the model string for Callisto has crap in it.... we
# should really have another entry in the vehicleinfo data
# to carry the path to the JSON.
actual_model = model.split(":")[0]
defaults = self.model_defaults_filepath(actual_model)
if not isinstance(defaults, list):
defaults = [defaults]
self.customise_SITL_commandline(
[],
defaults_filepath=defaults,
model=model,
wipe=True,
)
mission_file = "basic.txt"
quadplane = self.get_parameter('Q_ENABLE')
if quadplane:
mission_file = "basic-quadplane.txt"
tailsitter = self.get_parameter('Q_TAILSIT_ENABLE')
if tailsitter:
# tailsitter needs extra re-boot to pick up the rotated AHRS view
self.reboot_sitl()
self.wait_ready_to_arm()
self.arm_vehicle()
self.fly_mission(mission_file, strict=False, quadplane=quadplane, mission_timeout=400.0)
self.wait_disarmed()
def RCDisableAirspeedUse(self):
'''Test RC DisableAirspeedUse option'''
self.set_parameter("RC9_OPTION", 106)
self.delay_sim_time(5)
self.set_rc(9, 1000)
self.wait_sensor_state(
mavutil.mavlink.MAV_SYS_STATUS_SENSOR_DIFFERENTIAL_PRESSURE,
True,
True,
True)
self.set_rc(9, 2000)
self.wait_sensor_state(
mavutil.mavlink.MAV_SYS_STATUS_SENSOR_DIFFERENTIAL_PRESSURE,
True,
False,
True)
self.set_rc(9, 1000)
self.wait_sensor_state(
mavutil.mavlink.MAV_SYS_STATUS_SENSOR_DIFFERENTIAL_PRESSURE,
True,
True,
True)
def WatchdogHome(self):
'''Ensure home is restored after watchdog reset'''
if self.gdb:
# we end up signalling the wrong process. I think.
# Probably need to have a "sitl_pid()" method to get the
# ardupilot process's PID.
self.progress("######## Skipping WatchdogHome test under GDB")
return
ex = None
try:
self.progress("Enabling watchdog")
self.set_parameter("BRD_OPTIONS", 1 << 0)
self.reboot_sitl()
self.wait_ready_to_arm()
self.progress("Explicitly setting home to a known location")
orig_home = self.poll_home_position()
new_home = orig_home
new_home.latitude = new_home.latitude + 1000
new_home.longitude = new_home.longitude + 2000
new_home.altitude = new_home.altitude + 300000 # 300 metres
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_SET_HOME,
p5=new_home.latitude,
p6=new_home.longitude,
p7=new_home.altitude/1000.0, # mm => m
)
old_bootcount = self.get_parameter('STAT_BOOTCNT')
self.progress("Forcing watchdog reset")
os.kill(self.sitl.pid, signal.SIGALRM)
self.detect_and_handle_reboot(old_bootcount)
self.wait_statustext("WDG:")
self.wait_statustext("IMU1 is using GPS") # won't be come armable
self.progress("Verifying home position")
post_reboot_home = self.poll_home_position()
delta = self.get_distance_int(new_home, post_reboot_home)
max_delta = 1
if delta > max_delta:
raise NotAchievedException(
"New home not where it should be (dist=%f) (want=%s) (got=%s)" %
(delta, str(new_home), str(post_reboot_home)))
except Exception as e:
self.print_exception_caught(e)
ex = e
self.reboot_sitl()
if ex is not None:
raise ex
def AUTOTUNE(self):
'''Test AutoTune mode'''
self.takeoff(100)
self.change_mode('AUTOTUNE')
self.context_collect('STATUSTEXT')
tstart = self.get_sim_time()
axis = "Roll"
rc_value = 1000
while True:
timeout = 600
if self.get_sim_time() - tstart > timeout:
raise NotAchievedException("Did not complete within %u seconds" % timeout)
try:
m = self.wait_statustext("%s: Finished" % axis, check_context=True, timeout=0.1)
self.progress("Got %s" % str(m))
if axis == "Roll":
axis = "Pitch"
elif axis == "Pitch":
break
else:
raise ValueError("Bug: %s" % axis)
except AutoTestTimeoutException:
pass
self.delay_sim_time(1)
if rc_value == 1000:
rc_value = 2000
elif rc_value == 2000:
rc_value = 1000
elif rc_value == 1000:
rc_value = 2000
else:
raise ValueError("Bug")
if axis == "Roll":
self.set_rc(1, rc_value)
self.set_rc(2, 1500)
elif axis == "Pitch":
self.set_rc(1, 1500)
self.set_rc(2, rc_value)
else:
raise ValueError("Bug")
tdelta = self.get_sim_time() - tstart
self.progress("Finished in %0.1f seconds" % (tdelta,))
self.set_rc(1, 1500)
self.set_rc(2, 1500)
self.change_mode('FBWA')
self.fly_home_land_and_disarm(timeout=tdelta+240)
def AutotuneFiltering(self):
'''Test AutoTune mode with filter updates disabled'''
self.set_parameters({
"AUTOTUNE_OPTIONS": 3,
# some filtering is required for autotune to complete
"RLL_RATE_FLTD": 10,
"PTCH_RATE_FLTD": 10,
"RLL_RATE_FLTT": 20,
"PTCH_RATE_FLTT": 20,
})
self.AUTOTUNE()
def LandingDrift(self):
'''Circuit with baro drift'''
self.customise_SITL_commandline([], wipe=True)
self.set_analog_rangefinder_parameters()
self.set_parameters({
"SIM_BARO_DRIFT": -0.02,
"SIM_TERRAIN": 0,
"RNGFND_LANDING": 1,
"LAND_SLOPE_RCALC": 2,
"LAND_ABORT_DEG": 1,
})
self.reboot_sitl()
self.wait_ready_to_arm()
self.arm_vehicle()
# Load and start mission
self.load_mission("ap-circuit.txt", strict=True)
self.set_current_waypoint(1, check_afterwards=True)
self.change_mode('AUTO')
self.wait_current_waypoint(1, timeout=5)
self.wait_groundspeed(0, 10, timeout=5)
# Wait for landing waypoint
self.wait_current_waypoint(9, timeout=1200)
# Wait for landing restart
self.wait_current_waypoint(5, timeout=60)
# Wait for landing waypoint (second attempt)
self.wait_current_waypoint(9, timeout=1200)
self.wait_disarmed(timeout=180)
def DCMFallback(self):
'''Really annoy the EKF and force fallback'''
self.reboot_sitl()
self.delay_sim_time(30)
self.takeoff(50)
self.change_mode('CIRCLE')
self.context_push()
self.context_collect('STATUSTEXT')
self.set_parameters({
"EK3_POS_I_GATE": 0,
"SIM_GPS_HZ": 1,
"SIM_GPS_LAG_MS": 1000,
})
self.wait_statustext("DCM Active", check_context=True, timeout=60)
self.wait_statustext("EKF3 Active", check_context=True)
self.wait_statustext("DCM Active", check_context=True)
self.wait_statustext("EKF3 Active", check_context=True)
self.wait_statustext("DCM Active", check_context=True)
self.wait_statustext("EKF3 Active", check_context=True)
self.context_stop_collecting('STATUSTEXT')
self.fly_home_land_and_disarm()
self.context_pop()
self.reboot_sitl()
def ForcedDCM(self):
'''Switch to DCM mid-flight'''
self.wait_ready_to_arm()
self.arm_vehicle()
self.takeoff(50)
self.context_collect('STATUSTEXT')
self.set_parameter("AHRS_EKF_TYPE", 0)
self.wait_statustext("DCM Active", check_context=True)
self.context_stop_collecting('STATUSTEXT')
self.fly_home_land_and_disarm()
def EFITest(self, efi_type, name, sim_name, check_fuel_flow=True):
'''method to be called by EFI tests'''
self.start_subtest("EFI Test for (%s)" % name)
self.assert_not_receiving_message('EFI_STATUS')
self.set_parameters({
'SIM_EFI_TYPE': efi_type,
'EFI_TYPE': efi_type,
'SERIAL5_PROTOCOL': 24,
'RPM1_TYPE': 10,
})
self.customise_SITL_commandline(
["--serial5=sim:%s" % sim_name,
],
)
self.wait_ready_to_arm()
baro_m = self.assert_receive_message("SCALED_PRESSURE")
self.progress(self.dump_message_verbose(baro_m))
baro_temperature = baro_m.temperature / 100.0 # cDeg->deg
m = self.assert_received_message_field_values("EFI_STATUS", {
"throttle_out": 0,
"health": 1,
}, very_verbose=1)
if abs(baro_temperature - m.intake_manifold_temperature) > 1:
raise NotAchievedException(
"Bad intake manifold temperature (want=%f got=%f)" %
(baro_temperature, m.intake_manifold_temperature))
self.arm_vehicle()
self.set_rc(3, 1300)
tstart = self.get_sim_time()
while True:
now = self.get_sim_time_cached()
if now - tstart > 10:
raise NotAchievedException("RPM1 and EFI_STATUS.rpm did not match")
rpm_m = self.assert_receive_message("RPM", verbose=1)
want_rpm = 1000
if rpm_m.rpm1 < want_rpm:
continue
m = self.assert_receive_message("EFI_STATUS", verbose=1)
if abs(m.rpm - rpm_m.rpm1) > 100:
continue
break
self.progress("now we're started, check a few more values")
# note that megasquirt drver doesn't send throttle, so throttle_out is zero!
m = self.assert_received_message_field_values("EFI_STATUS", {
"health": 1,
}, very_verbose=1)
m = self.wait_message_field_values("EFI_STATUS", {
"throttle_position": 31,
"intake_manifold_temperature": 28,
}, very_verbose=1, epsilon=2)
if check_fuel_flow:
if abs(m.fuel_flow - 0.2) < 0.0001:
raise NotAchievedException("Expected fuel flow")
self.set_rc(3, 1000)
# need to force disarm as the is_flying flag can trigger with the engine running
self.disarm_vehicle(force=True)
def MegaSquirt(self):
'''test MegaSquirt driver'''
self.EFITest(
1, "MegaSquirt", "megasquirt",
check_fuel_flow=False,
)
def Hirth(self):
'''Test Hirth EFI'''
self.EFITest(8, "Hirth", "hirth")
def GlideSlopeThresh(self):
'''Test rebuild glide slope if above and climbing'''
# Test that GLIDE_SLOPE_THRESHOLD correctly controls re-planning glide slope
# in the scenario that aircraft is above planned slope and slope is positive (climbing).
#
#
# Behaviour with GLIDE_SLOPE_THRESH = 0 (no slope replanning)
# (2).. __(4)
# | \..__/
# | __/
# (3)
#
# Behaviour with GLIDE_SLOPE_THRESH = 5 (slope replanning when >5m error)
# (2)........__(4)
# | __/
# | __/
# (3)
# Solid is plan, dots are actual flightpath.
self.load_mission('rapid-descent-then-climb.txt', strict=False)
self.set_current_waypoint(1)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
#
# Initial run with GLIDE_SLOPE_THR = 5 (default).
#
self.set_parameter("GLIDE_SLOPE_THR", 5)
# Wait for waypoint commanding rapid descent, followed by climb.
self.wait_current_waypoint(5, timeout=1200)
# Altitude should not descend significantly below the initial altitude
init_altitude = self.get_altitude(relative=True, timeout=2)
timeout = 600
wpnum = 7
tstart = self.get_sim_time()
while True:
if self.get_sim_time() - tstart > timeout:
raise AutoTestTimeoutException("Did not get wanted current waypoint")
if (self.get_altitude(relative=True, timeout=2) - init_altitude) < -10:
raise NotAchievedException("Descended >10m before reaching desired waypoint,\
indicating slope was not replanned")
seq = self.mav.waypoint_current()
self.progress("Waiting for wp=%u current=%u" % (wpnum, seq))
if seq == wpnum:
break
self.set_current_waypoint(2)
#
# Second run with GLIDE_SLOPE_THR = 0 (no re-plan).
#
self.set_parameter("GLIDE_SLOPE_THR", 0)
# Wait for waypoint commanding rapid descent, followed by climb.
self.wait_current_waypoint(5, timeout=1200)
# This time altitude should descend significantly below the initial altitude
init_altitude = self.get_altitude(relative=True, timeout=2)
timeout = 600
wpnum = 7
tstart = self.get_sim_time()
while True:
if self.get_sim_time() - tstart > timeout:
raise AutoTestTimeoutException("Did not get wanted altitude")
seq = self.mav.waypoint_current()
self.progress("Waiting for wp=%u current=%u" % (wpnum, seq))
if seq == wpnum:
raise NotAchievedException("Reached desired waypoint without first decending 10m,\
indicating slope was replanned unexpectedly")
if (self.get_altitude(relative=True, timeout=2) - init_altitude) < -10:
break
# Disarm
self.wait_disarmed(timeout=600)
self.progress("Mission OK")
def MAV_CMD_NAV_LOITER_TURNS(self, target_system=1, target_component=1):
'''test MAV_CMD_NAV_LOITER_TURNS mission item'''
alt = 100
seq = 0
items = []
tests = [
(self.home_relative_loc_ne(50, -50), 100, 0.3),
(self.home_relative_loc_ne(100, 50), 1005, 3),
]
# add a home position:
items.append(self.mav.mav.mission_item_int_encode(
target_system,
target_component,
seq, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_NAV_WAYPOINT,
0, # current
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0, # longitude
0, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION))
seq += 1
# add takeoff
items.append(self.mav.mav.mission_item_int_encode(
target_system,
target_component,
seq, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT,
mavutil.mavlink.MAV_CMD_NAV_TAKEOFF,
0, # current
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0, # longitude
alt, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION))
seq += 1
# add circles
for (loc, radius, turn) in tests:
items.append(self.mav.mav.mission_item_int_encode(
target_system,
target_component,
seq, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT,
mavutil.mavlink.MAV_CMD_NAV_LOITER_TURNS,
0, # current
0, # autocontinue
turn, # p1
0, # p2
radius, # p3
0, # p4
int(loc.lat*1e7), # latitude
int(loc.lng*1e7), # longitude
alt, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION))
seq += 1
# add an RTL
items.append(self.mav.mav.mission_item_int_encode(
target_system,
target_component,
seq, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_NAV_RETURN_TO_LAUNCH,
0, # current
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0, # longitude
0, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION))
seq += 1
self.upload_using_mission_protocol(mavutil.mavlink.MAV_MISSION_TYPE_MISSION, items)
downloaded_items = self.download_using_mission_protocol(mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
ofs = 2
self.progress("Checking downloaded mission is as expected")
for (loc, radius, turn) in tests:
downloaded = downloaded_items[ofs]
if radius > 255:
# ArduPilot only stores % 10
radius = radius - radius % 10
if downloaded.param3 != radius:
raise NotAchievedException(
"Did not get expected radius for item %u; want=%f got=%f" %
(ofs, radius, downloaded.param3))
if turn > 0 and turn < 1:
# ArduPilot stores fractions in 8 bits (*256) and unpacks it (/256)
turn = int(turn*256) / 256.0
if downloaded.param1 != turn:
raise NotAchievedException(
"Did not get expected turn for item %u; want=%f got=%f" %
(ofs, turn, downloaded.param1))
ofs += 1
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.set_parameter("NAVL1_LIM_BANK", 50)
self.wait_current_waypoint(2)
for (loc, expected_radius, _) in tests:
self.wait_circling_point_with_radius(
loc,
expected_radius,
epsilon=20.0,
timeout=240,
)
self.set_current_waypoint(self.current_waypoint()+1)
self.fly_home_land_and_disarm(timeout=180)
def MidAirDisarmDisallowed(self):
'''Ensure mid-air disarm is not possible'''
self.takeoff(50)
disarmed = False
try:
self.disarm_vehicle()
disarmed = True
except ValueError as e:
self.progress("Got %s" % repr(e))
if "Expected MAV_RESULT_ACCEPTED got MAV_RESULT_FAILED" not in str(e):
raise e
if disarmed:
raise NotAchievedException("Disarmed when we shouldn't have")
# should still be able to force-disarm:
self.disarm_vehicle(force=True)
self.reboot_sitl()
def AerobaticsScripting(self):
'''Fixed Wing Aerobatics'''
applet_script = "Aerobatics/FixedWing/plane_aerobatics.lua"
airshow = "Aerobatics/FixedWing/Schedules/AirShow.txt"
trick72 = "trick72.txt"
model = "plane-3d"
self.customise_SITL_commandline(
[],
model=model,
defaults_filepath="Tools/autotest/models/plane-3d.parm",
wipe=True)
self.context_push()
self.install_applet_script(applet_script)
self.install_applet_script(airshow, install_name=trick72)
self.context_collect('STATUSTEXT')
self.reboot_sitl()
self.set_parameter("TRIK_ENABLE", 1)
self.set_rc(7, 1000) # disable tricks
self.scripting_restart()
self.wait_text("Enabled 3 aerobatic tricks", check_context=True)
self.set_parameters({
"TRIK1_ID": 72,
"RC7_OPTION" : 300, # activation switch
"RC9_OPTION" : 301, # selection switch
"SIM_SPEEDUP": 5, # need to give some cycles to lua
})
self.wait_ready_to_arm()
self.change_mode("TAKEOFF")
self.arm_vehicle()
self.wait_altitude(30, 40, timeout=30, relative=True)
self.change_mode("CRUISE")
self.set_rc(9, 1000) # select first trick
self.delay_sim_time(1)
self.set_rc(7, 1500) # show selected trick
self.wait_text("Trick 1 selected (SuperAirShow)", check_context=True)
self.set_rc(7, 2000) # activate trick
self.wait_text("Trick 1 started (SuperAirShow)", check_context=True)
highest_error = 0
while True:
m = self.mav.recv_match(type='NAMED_VALUE_FLOAT', blocking=True, timeout=2)
if not m:
break
if m.name != 'PERR':
continue
highest_error = max(highest_error, m.value)
if highest_error > 15:
raise NotAchievedException("path error %.1f" % highest_error)
if highest_error == 0:
raise NotAchievedException("path error not reported")
self.progress("Finished trick, max error=%.1fm" % highest_error)
self.disarm_vehicle(force=True)
self.remove_installed_script(applet_script)
self.remove_installed_script(trick72)
messages = self.context_collection('STATUSTEXT')
self.context_pop()
self.reboot_sitl()
# check all messages to see if we got all tricks
tricks = ["Loop", "HalfReverseCubanEight", "ScaleFigureEight", "Immelmann",
"Split-S", "RollingCircle", "HumptyBump", "HalfCubanEight",
"BarrelRoll", "CrossBoxTopHat", "TriangularLoop",
"Finishing SuperAirShow!"]
texts = [m.text for m in messages]
for t in tricks:
if t in texts:
self.progress("Completed trick %s" % t)
else:
raise NotAchievedException("Missing trick %s" % t)
def SDCardWPTest(self):
'''test BRD_SD_MISSION support'''
spiral_script = "mission_spiral.lua"
self.context_push()
self.install_example_script(spiral_script)
self.context_collect('STATUSTEXT')
self.set_parameters({
"BRD_SD_MISSION" : 64,
"SCR_ENABLE" : 1,
"SCR_VM_I_COUNT" : 1000000
})
self.wait_ready_to_arm()
self.reboot_sitl()
self.wait_text("Loaded spiral mission creator", check_context=True)
self.set_parameters({
"SCR_USER2": 19, # radius
"SCR_USER3": -35.36322, # lat
"SCR_USER4": 149.16525, # lon
"SCR_USER5": 684.13, # alt
})
count = (65536 // 15) - 1
self.progress("Creating spiral mission of size %s" % count)
self.set_parameter("SCR_USER1", count)
self.wait_text("Created spiral of size %u" % count, check_context=True)
self.progress("Checking spiral before reboot")
self.set_parameter("SCR_USER6", count)
self.wait_text("Compared spiral of size %u OK" % count, check_context=True)
self.set_parameter("SCR_USER6", 0)
self.wait_ready_to_arm()
self.reboot_sitl()
self.progress("Checking spiral after reboot")
self.set_parameter("SCR_USER6", count)
self.wait_text("Compared spiral of size %u OK" % count, check_context=True)
self.remove_installed_script(spiral_script)
self.context_pop()
self.wait_ready_to_arm()
self.reboot_sitl()
def MANUAL_CONTROL(self):
'''test MANUAL_CONTROL mavlink message'''
self.set_parameter("SYSID_MYGCS", self.mav.source_system)
self.progress("Takeoff")
self.takeoff(alt=50)
self.change_mode('FBWA')
tstart = self.get_sim_time_cached()
roll_input = -500
want_roll_degrees = -12
while True:
if self.get_sim_time_cached() - tstart > 10:
raise AutoTestTimeoutException("Did not reach roll")
self.progress("Sending roll-left")
self.mav.mav.manual_control_send(
1, # target system
32767, # x (pitch)
roll_input, # y (roll)
32767, # z (thrust)
32767, # r (yaw)
0) # button mask
m = self.mav.recv_match(type='ATTITUDE', blocking=True, timeout=1)
print("m=%s" % str(m))
if m is None:
continue
p = math.degrees(m.roll)
self.progress("roll=%f want<=%f" % (p, want_roll_degrees))
if p <= want_roll_degrees:
break
self.mav.mav.manual_control_send(
1, # target system
32767, # x (pitch)
32767, # y (roll)
32767, # z (thrust)
32767, # r (yaw)
0) # button mask
self.fly_home_land_and_disarm()
def mission_home_point(self, target_system=1, target_component=1):
'''just an empty-ish item-int to store home'''
return self.mav.mav.mission_item_int_encode(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_NAV_WAYPOINT,
0, # current
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0, # longitude
0, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
def mission_jump_tag(self, tag, target_system=1, target_component=1):
'''create a jump tag mission item'''
return self.mav.mav.mission_item_int_encode(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_JUMP_TAG,
0, # current
0, # autocontinue
tag, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0, # longitude
0, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
def mission_do_jump_tag(self, tag, target_system=1, target_component=1):
'''create a jump tag mission item'''
return self.mav.mav.mission_item_int_encode(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_DO_JUMP_TAG,
0, # current
0, # autocontinue
tag, # p1
0, # p2
0, # p3
0, # p4
0, # latitude
0, # longitude
0, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
def mission_anonymous_waypoint(self, target_system=1, target_component=1):
'''just a boring waypoint'''
return self.mav.mav.mission_item_int_encode(
target_system,
target_component,
0, # seq
mavutil.mavlink.MAV_FRAME_GLOBAL,
mavutil.mavlink.MAV_CMD_NAV_WAYPOINT,
0, # current
0, # autocontinue
0, # p1
0, # p2
0, # p3
0, # p4
1, # latitude
1, # longitude
1, # altitude
mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
def renumber_mission_items(self, mission):
count = 0
for item in mission:
item.seq = count
count += 1
def MissionJumpTags_missing_jump_target(self, target_system=1, target_component=1):
self.start_subtest("Check missing-jump-tag behaviour")
jump_target = 2
mission = [
self.mission_home_point(),
self.mission_anonymous_waypoint(),
self.mission_anonymous_waypoint(),
self.mission_jump_tag(jump_target),
self.mission_anonymous_waypoint(),
self.mission_anonymous_waypoint(),
]
self.renumber_mission_items(mission)
self.check_mission_upload_download(mission)
self.progress("Checking incorrect tag behaviour")
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_JUMP_TAG,
p1=jump_target + 1,
want_result=mavutil.mavlink.MAV_RESULT_FAILED
)
self.progress("Checking correct tag behaviour")
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_JUMP_TAG,
p1=jump_target,
)
self.assert_current_waypoint(4)
def MissionJumpTags_do_jump_to_bad_tag(self, target_system=1, target_component=1):
mission = [
self.mission_home_point(),
self.mission_anonymous_waypoint(),
self.mission_do_jump_tag(17),
self.mission_anonymous_waypoint(),
]
self.renumber_mission_items(mission)
self.check_mission_upload_download(mission)
self.change_mode('AUTO')
self.arm_vehicle()
self.set_current_waypoint(2, check_afterwards=False)
self.assert_mode('RTL')
self.disarm_vehicle()
def MissionJumpTags_jump_tag_at_end_of_mission(self, target_system=1, target_component=1):
mission = [
self.mission_home_point(),
self.mission_anonymous_waypoint(),
self.mission_jump_tag(17),
]
# Jumping to an end of a mission, either DO_JUMP or DO_JUMP_TAG will result in a failed attempt.
# The failure is from mission::set_current_cmd() returning false if it can not find any NAV
# commands on or after the index. Two scenarios:
# 1) AUTO mission triggered: The the set_command will fail and it will cause an RTL event
# (Harder to test, need vehicle to actually reach the waypoint)
# 2) GCS/MAVLink: It will return MAV_RESULT_FAILED and there's on change to the mission. (Easy to test)
self.renumber_mission_items(mission)
self.check_mission_upload_download(mission)
self.progress("Checking correct tag behaviour")
self.change_mode('AUTO')
self.arm_vehicle()
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_JUMP_TAG,
p1=17,
want_result=mavutil.mavlink.MAV_RESULT_FAILED
)
self.disarm_vehicle()
def MissionJumpTags(self):
'''test MAV_CMD_JUMP_TAG'''
self.wait_ready_to_arm()
self.MissionJumpTags_missing_jump_target()
self.MissionJumpTags_do_jump_to_bad_tag()
self.MissionJumpTags_jump_tag_at_end_of_mission()
def AltResetBadGPS(self):
'''Tests the handling of poor GPS lock pre-arm alt resets'''
self.set_parameters({
"SIM_GPS_GLITCH_Z": 0,
"SIM_GPS_ACC": 0.3,
})
self.wait_ready_to_arm()
m = self.assert_receive_message('GLOBAL_POSITION_INT')
relalt = m.relative_alt*0.001
if abs(relalt) > 3:
raise NotAchievedException("Bad relative alt %.1f" % relalt)
self.progress("Setting low accuracy, glitching GPS")
self.set_parameter("SIM_GPS_ACC", 40)
self.set_parameter("SIM_GPS_GLITCH_Z", -47)
self.progress("Waiting 10s for height update")
self.delay_sim_time(10)
self.wait_ready_to_arm()
self.arm_vehicle()
m = self.assert_receive_message('GLOBAL_POSITION_INT')
relalt = m.relative_alt*0.001
if abs(relalt) > 3:
raise NotAchievedException("Bad glitching relative alt %.1f" % relalt)
self.disarm_vehicle()
# reboot to clear potentially bad state
def trigger_airspeed_cal(self):
self.run_cmd(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p3=1,
)
def AirspeedCal(self):
'''test Airspeed calibration'''
self.start_subtest('1 airspeed sensor')
self.context_push()
self.context_collect('STATUSTEXT')
self.trigger_airspeed_cal()
self.wait_statustext('Airspeed 1 calibrated', check_context=True)
self.context_pop()
self.context_push()
self.context_collect('STATUSTEXT')
self.start_subtest('0 airspeed sensors')
self.set_parameter('ARSPD_TYPE', 0)
self.reboot_sitl()
self.wait_statustext('No airspeed sensor', check_context=True)
self.trigger_airspeed_cal()
self.delay_sim_time(5)
if self.statustext_in_collections('Airspeed 1 calibrated'):
raise NotAchievedException("Did not disable airspeed sensor?!")
self.context_pop()
self.start_subtest('2 airspeed sensors')
self.set_parameter('ARSPD_TYPE', 100)
self.set_parameter('ARSPD2_TYPE', 100)
self.reboot_sitl()
self.context_push()
self.context_collect('STATUSTEXT')
self.trigger_airspeed_cal()
self.wait_statustext('Airspeed 1 calibrated', check_context=True)
self.wait_statustext('Airspeed 2 calibrated', check_context=True)
self.context_pop()
self.reboot_sitl()
def RunMissionScript(self):
'''Test run_mission.py script'''
script = os.path.join('Tools', 'autotest', 'run_mission.py')
self.stop_SITL()
util.run_cmd([
util.reltopdir(script),
self.binary,
'plane',
self.generic_mission_filepath_for_filename("flaps.txt"),
])
self.start_SITL()
def MAV_CMD_GUIDED_CHANGE_ALTITUDE(self):
'''test handling of MAV_CMD_GUIDED_CHANGE_ALTITUDE'''
self.takeoff(30, relative=True)
self.change_mode('GUIDED')
for alt in 50, 70:
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_GUIDED_CHANGE_ALTITUDE,
p7=alt,
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT,
)
self.wait_altitude(alt-1, alt+1, timeout=30, relative=True)
# test for #24535
self.change_mode('LOITER')
self.delay_sim_time(5)
self.change_mode('GUIDED')
self.wait_altitude(
alt-3, # NOTE: reuse of alt from above loop!
alt+3,
minimum_duration=10,
timeout=30,
relative=True,
)
self.fly_home_land_and_disarm()
def _MAV_CMD_PREFLIGHT_CALIBRATION(self, command):
self.context_push()
self.start_subtest("Denied when armed")
self.wait_ready_to_arm()
self.arm_vehicle()
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p1=1,
want_result=mavutil.mavlink.MAV_RESULT_FAILED,
)
self.disarm_vehicle()
self.context_collect('STATUSTEXT')
self.start_subtest("gyro cal")
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p1=1,
)
self.start_subtest("baro cal")
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p3=1,
)
self.wait_statustext('Barometer calibration complete', check_context=True)
# accelcal skipped here, it is checked elsewhere
self.start_subtest("ins trim")
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=2,
)
# enforced delay between cals:
self.delay_sim_time(5)
self.start_subtest("simple accel cal")
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=4,
)
# simple gyro cal makes the GPS units go unhealthy as they are
# not maintaining their update rate (gyro cal is synchronous
# in the main loop). Usually ~30 seconds to recover...
self.wait_gps_sys_status_not_present_or_enabled_and_healthy(timeout=60)
self.start_subtest("force save accels")
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p5=76,
)
self.start_subtest("force save compasses")
command(
mavutil.mavlink.MAV_CMD_PREFLIGHT_CALIBRATION,
p2=76,
)
self.context_pop()
def MAV_CMD_PREFLIGHT_CALIBRATION(self):
'''test MAV_CMD_PREFLIGHT_CALIBRATION mavlink handling'''
self._MAV_CMD_PREFLIGHT_CALIBRATION(self.run_cmd)
self._MAV_CMD_PREFLIGHT_CALIBRATION(self.run_cmd_int)
def MAV_CMD_DO_INVERTED_FLIGHT(self):
'''fly upside-down mission item'''
alt = 30
wps = self.create_simple_relhome_mission([
(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, 0, 0, alt),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 400, 0, alt),
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_DO_INVERTED_FLIGHT,
p1=1,
),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 800, 0, alt),
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_DO_INVERTED_FLIGHT,
p1=0,
),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 1200, 0, alt),
(mavutil.mavlink.MAV_CMD_NAV_RETURN_TO_LAUNCH, 0, 0, 0),
])
self.check_mission_upload_download(wps)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_current_waypoint(2) # upright flight
self.wait_message_field_values("NAV_CONTROLLER_OUTPUT", {
"nav_roll": 0,
"nav_pitch": 0,
}, epsilon=10)
def check_altitude(mav, m):
global initial_airspeed_threshold_reached
m_type = m.get_type()
if m_type != 'GLOBAL_POSITION_INT':
return
if abs(30 - m.relative_alt * 0.001) > 15:
raise NotAchievedException("Bad altitude while flying inverted")
self.context_push()
self.install_message_hook_context(check_altitude)
self.wait_current_waypoint(4) # inverted flight
self.wait_message_field_values("NAV_CONTROLLER_OUTPUT", {
"nav_roll": 180,
"nav_pitch": 9,
}, epsilon=10,)
self.wait_current_waypoint(6) # upright flight
self.wait_message_field_values("NAV_CONTROLLER_OUTPUT", {
"nav_roll": 0,
"nav_pitch": 0,
}, epsilon=10)
self.context_pop() # remove the check_altitude call
self.wait_current_waypoint(7)
self.fly_home_land_and_disarm()
def MAV_CMD_DO_AUTOTUNE_ENABLE(self):
'''test enabling autotune via mavlink'''
self.context_collect('STATUSTEXT')
self.run_cmd(mavutil.mavlink.MAV_CMD_DO_AUTOTUNE_ENABLE, p1=1)
self.wait_statustext('Started autotune', check_context=True)
self.run_cmd_int(mavutil.mavlink.MAV_CMD_DO_AUTOTUNE_ENABLE, p1=0)
self.wait_statustext('Stopped autotune', check_context=True)
def DO_PARACHUTE(self):
'''test triggering parachute via mavlink'''
self.set_parameters({
"CHUTE_ENABLED": 1,
"CHUTE_TYPE": 10,
"SERVO9_FUNCTION": 27,
"SIM_PARA_ENABLE": 1,
"SIM_PARA_PIN": 9,
"FS_LONG_ACTN": 3,
})
for command in self.run_cmd, self.run_cmd_int:
self.wait_servo_channel_value(9, 1100)
self.wait_ready_to_arm()
self.arm_vehicle()
command(
mavutil.mavlink.MAV_CMD_DO_PARACHUTE,
p1=mavutil.mavlink.PARACHUTE_RELEASE,
)
self.wait_servo_channel_value(9, 1300)
self.disarm_vehicle()
self.reboot_sitl()
def _MAV_CMD_DO_GO_AROUND(self, command):
self.load_mission("mission.txt")
self.set_parameter("RTL_AUTOLAND", 3)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_current_waypoint(6)
command(mavutil.mavlink.MAV_CMD_DO_GO_AROUND, p1=150)
self.wait_current_waypoint(5)
self.wait_altitude(135, 165, relative=True)
self.wait_disarmed(timeout=300)
def MAV_CMD_DO_GO_AROUND(self):
'''test MAV_CMD_DO_GO_AROUND as a mavlink command'''
self._MAV_CMD_DO_GO_AROUND(self.run_cmd)
self._MAV_CMD_DO_GO_AROUND(self.run_cmd_int)
def _MAV_CMD_DO_FLIGHTTERMINATION(self, command):
self.set_parameters({
"AFS_ENABLE": 1,
"SYSID_MYGCS": self.mav.source_system,
"AFS_TERM_ACTION": 42,
})
self.wait_ready_to_arm()
self.arm_vehicle()
self.context_collect('STATUSTEXT')
command(mavutil.mavlink.MAV_CMD_DO_FLIGHTTERMINATION, p1=1)
self.wait_disarmed()
self.wait_text('Terminating due to GCS request', check_context=True)
self.reboot_sitl()
def MAV_CMD_DO_FLIGHTTERMINATION(self):
'''test MAV_CMD_DO_FLIGHTTERMINATION works on Plane'''
self._MAV_CMD_DO_FLIGHTTERMINATION(self.run_cmd)
self._MAV_CMD_DO_FLIGHTTERMINATION(self.run_cmd_int)
def MAV_CMD_DO_LAND_START(self):
'''test MAV_CMD_DO_LAND_START as mavlink command'''
self.set_parameters({
"RTL_AUTOLAND": 3,
})
self.upload_simple_relhome_mission([
(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, 0, 0, 30),
(mavutil.mavlink.MAV_CMD_NAV_LOITER_UNLIM, 0, 0, 30),
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_DO_LAND_START,
),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 800, 0, 0),
])
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.start_subtest("DO_LAND_START as COMMAND_LONG")
self.wait_current_waypoint(2)
self.run_cmd(mavutil.mavlink.MAV_CMD_DO_LAND_START)
self.wait_current_waypoint(4)
self.start_subtest("DO_LAND_START as COMMAND_INT")
self.set_current_waypoint(2)
self.run_cmd_int(mavutil.mavlink.MAV_CMD_DO_LAND_START)
self.wait_current_waypoint(4)
self.fly_home_land_and_disarm()
def MAV_CMD_NAV_ALTITUDE_WAIT(self):
'''test MAV_CMD_NAV_ALTITUDE_WAIT mission item, wiggling only'''
# Load a single waypoint
self.upload_simple_relhome_mission([
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_NAV_ALTITUDE_WAIT,
p1=1000, # 1000m alt threshold, this should not trigger
p2=10, # 10m/s descent rate, this should not trigger
p3=10 # servo wiggle every 10 seconds
)
])
def look_for_wiggle(mav, m):
if m.get_type() == 'SERVO_OUTPUT_RAW':
# Throttle must be zero
if m.servo3_raw != 1000:
raise NotAchievedException(
"Throttle must be 0 in altitude wait, got %f" % m.servo3_raw)
# Aileron, elevator and rudder must all be the same
# However, aileron is revered, so we must un-reverse it
value = 1500 - (m.servo1_raw - 1500)
if (m.servo2_raw != value) or (m.servo4_raw != value):
raise NotAchievedException(
"Aileron, elevator and rudder must be the same")
# Start mission
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
# Check outputs
self.context_push()
self.install_message_hook_context(look_for_wiggle)
# Wait for a bit to let message hook sample
self.delay_sim_time(60)
self.context_pop()
# If the mission item completes as there is no other waypoints we will end up in RTL
if not self.mode_is('AUTO'):
raise NotAchievedException("Must still be in AUTO")
self.disarm_vehicle()
def start_flying_simple_rehome_mission(self, items):
'''uploads items, changes mode to auto, waits ready to arm and arms
vehicle. If the first item it a takeoff you can expect the
vehicle to fly after this method returns
'''
self.upload_simple_relhome_mission(items)
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
def InteractTest(self):
'''just takeoff'''
if self.mavproxy is None:
raise NotAchievedException("Must be started with --map")
self.start_flying_simple_rehome_mission([
(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, 0, 0, 30),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 800, 0, 0),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 800, 800, 0),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 0, 400, 0),
])
self.wait_current_waypoint(4)
self.set_parameter('SIM_SPEEDUP', 1)
self.mavproxy.interact()
def MAV_CMD_MISSION_START(self):
'''test MAV_CMD_MISSION_START starts AUTO'''
self.upload_simple_relhome_mission([
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 800, 0, 0),
])
for run_cmd in self.run_cmd, self.run_cmd_int:
self.change_mode('LOITER')
run_cmd(mavutil.mavlink.MAV_CMD_MISSION_START)
self.wait_mode('AUTO')
def MAV_CMD_NAV_LOITER_UNLIM(self):
'''test receiving MAV_CMD_NAV_LOITER_UNLIM from GCS'''
self.takeoff(10)
self.run_cmd(mavutil.mavlink.MAV_CMD_NAV_LOITER_UNLIM)
self.wait_mode('LOITER')
self.change_mode('GUIDED')
self.run_cmd_int(mavutil.mavlink.MAV_CMD_NAV_LOITER_UNLIM)
self.wait_mode('LOITER')
self.fly_home_land_and_disarm()
def MAV_CMD_NAV_RETURN_TO_LAUNCH(self):
'''test receiving MAV_CMD_NAV_RETURN_TO_LAUNCH from GCS'''
self.set_parameter('RTL_AUTOLAND', 1)
self.start_flying_simple_rehome_mission([
(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, 0, 0, 30),
(mavutil.mavlink.MAV_CMD_NAV_LOITER_UNLIM, 0, 0, 30),
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_DO_LAND_START,
),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 800, 0, 0),
])
for i in self.run_cmd, self.run_cmd_int:
self.wait_current_waypoint(2)
self.run_cmd(mavutil.mavlink.MAV_CMD_NAV_RETURN_TO_LAUNCH)
self.wait_current_waypoint(4)
self.set_current_waypoint(2)
self.fly_home_land_and_disarm()
def location_from_ADSB_VEHICLE(self, m):
'''return a mavutil.location extracted from an ADSB_VEHICLE mavlink
message'''
if m.altitude_type != mavutil.mavlink.ADSB_ALTITUDE_TYPE_GEOMETRIC:
raise ValueError("Expected geometric alt")
return mavutil.location(
m.lat*1e-7,
m.lon*1e-7,
m.altitude/1000.0585, # mm -> m
m.heading * 0.01 # centidegrees -> degrees
)
def SagetechMXS(self):
'''test Sagetech MXS ADSB device driver'''
sim_name = "sagetech_mxs"
self.set_parameters({
"SERIAL5_PROTOCOL": 35,
"ADSB_TYPE": 4, # Sagetech-MXS
"SIM_ADSB_TYPES": 8, # Sagetech-MXS
"SIM_ADSB_COUNT": 5,
})
self.customise_SITL_commandline(["--serial5=sim:%s" % sim_name])
m = self.assert_receive_message("ADSB_VEHICLE")
adsb_vehicle_loc = self.location_from_ADSB_VEHICLE(m)
self.progress("ADSB Vehicle at loc %s" % str(adsb_vehicle_loc))
home = self.home_position_as_mav_location()
self.assert_distance(home, adsb_vehicle_loc, 0, 10000)
def MinThrottle(self):
'''Make sure min throttle does not apply in manual mode and does in FBWA'''
servo_min = self.get_parameter("RC3_MIN")
servo_max = self.get_parameter("RC3_MAX")
min_throttle = 10
servo_min_throttle = servo_min + (servo_max - servo_min) * (min_throttle / 100)
# Set min throttle
self.set_parameter('THR_MIN', min_throttle)
# Should be 0 throttle while disarmed
self.change_mode("MANUAL")
self.drain_mav() # make sure we have the latest data before checking throttle output
self.assert_servo_channel_value(3, servo_min)
# Arm and check throttle is still 0 in manual
self.wait_ready_to_arm()
self.arm_vehicle()
self.drain_mav()
self.assert_servo_channel_value(3, servo_min)
# FBWA should apply throttle min
self.change_mode("FBWA")
self.drain_mav()
self.assert_servo_channel_value(3, servo_min_throttle)
# But not when disarmed
self.disarm_vehicle()
self.drain_mav()
self.assert_servo_channel_value(3, servo_min)
def ClimbThrottleSaturation(self):
'''check what happens when throttle is saturated in GUIDED'''
self.set_parameters({
"TECS_CLMB_MAX": 30,
"TKOFF_ALT": 1000,
})
self.change_mode("TAKEOFF")
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_message_field_values('VFR_HUD', {
"throttle": 100,
}, minimum_duration=30, timeout=90)
self.disarm_vehicle(force=True)
self.reboot_sitl()
def tests(self):
'''return list of all tests'''
ret = super(AutoTestPlane, self).tests()
ret.extend([
self.AuxModeSwitch,
self.TestRCCamera,
self.TestRCRelay,
self.ThrottleFailsafe,
self.NeedEKFToArm,
self.ThrottleFailsafeFence,
self.TestFlaps,
self.DO_CHANGE_SPEED,
self.DO_REPOSITION,
self.GuidedRequest,
self.MainFlight,
self.TestGripperMission,
self.Parachute,
self.ParachuteSinkRate,
self.DO_PARACHUTE,
self.PitotBlockage,
self.AIRSPEED_AUTOCAL,
self.RangeFinder,
self.FenceStatic,
self.FenceRTL,
self.FenceRTLRally,
self.FenceRetRally,
self.FenceAltCeilFloor,
self.FenceBreachedChangeMode,
self.FenceNoFenceReturnPoint,
self.FenceNoFenceReturnPointInclusion,
self.FenceDisableUnderAction,
self.ADSB,
self.SimADSB,
self.Button,
self.FRSkySPort,
self.FRSkyPassThroughStatustext,
self.FRSkyPassThroughSensorIDs,
self.FRSkyMAVlite,
self.FRSkyD,
self.LTM,
self.DEVO,
self.AdvancedFailsafe,
self.LOITER,
self.MAV_CMD_NAV_LOITER_TURNS,
self.DeepStall,
self.WatchdogHome,
self.LargeMissions,
self.Soaring,
self.Terrain,
self.TerrainMission,
self.TerrainLoiter,
self.VectorNavEAHRS,
self.MicroStrainEAHRS5,
self.MicroStrainEAHRS7,
self.InertialLabsEAHRS,
self.GpsSensorPreArmEAHRS,
self.Deadreckoning,
self.DeadreckoningNoAirSpeed,
self.EKFlaneswitch,
self.AirspeedDrivers,
self.RTL_CLIMB_MIN,
self.ClimbBeforeTurn,
self.IMUTempCal,
self.MAV_CMD_DO_AUX_FUNCTION,
self.SmartBattery,
self.FlyEachFrame,
self.RCDisableAirspeedUse,
self.AHRS_ORIENTATION,
self.AHRSTrim,
self.LandingDrift,
self.ForcedDCM,
self.DCMFallback,
self.MAVFTP,
self.AUTOTUNE,
self.AutotuneFiltering,
self.MegaSquirt,
self.Hirth,
self.MSP_DJI,
self.SpeedToFly,
self.GlideSlopeThresh,
self.HIGH_LATENCY2,
self.MidAirDisarmDisallowed,
self.AerobaticsScripting,
self.MANUAL_CONTROL,
self.RunMissionScript,
self.WindEstimates,
self.AltResetBadGPS,
self.AirspeedCal,
self.MissionJumpTags,
Test(self.GCSFailsafe, speedup=8),
self.SDCardWPTest,
self.NoArmWithoutMissionItems,
self.MODE_SWITCH_RESET,
self.ExternalPositionEstimate,
self.SagetechMXS,
self.MAV_CMD_GUIDED_CHANGE_ALTITUDE,
self.MAV_CMD_PREFLIGHT_CALIBRATION,
self.MAV_CMD_DO_INVERTED_FLIGHT,
self.MAV_CMD_DO_AUTOTUNE_ENABLE,
self.MAV_CMD_DO_GO_AROUND,
self.MAV_CMD_DO_FLIGHTTERMINATION,
self.MAV_CMD_DO_LAND_START,
self.MAV_CMD_NAV_ALTITUDE_WAIT,
self.InteractTest,
self.MAV_CMD_MISSION_START,
self.TerrainRally,
self.MAV_CMD_NAV_LOITER_UNLIM,
self.MAV_CMD_NAV_RETURN_TO_LAUNCH,
self.MinThrottle,
self.ClimbThrottleSaturation,
])
return ret
def disabled_tests(self):
return {
"LandingDrift": "Flapping test. See https://github.com/ArduPilot/ardupilot/issues/20054",
"InteractTest": "requires user interaction",
"ClimbThrottleSaturation": "requires https://github.com/ArduPilot/ardupilot/pull/27106 to pass",
}
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