ardupilot/Tools/autotest/arduplane.py

1661 lines
63 KiB
Python
Raw Normal View History

#!/usr/bin/env python
# Fly ArduPlane in SITL
2016-11-08 07:06:05 -04:00
from __future__ import print_function
import math
import os
from pymavlink import quaternion
2013-06-18 03:27:21 -03:00
from pymavlink import mavutil
from common import AutoTest
from common import AutoTestTimeoutException
from common import NotAchievedException
from common import PreconditionFailedException
# 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(AutoTest):
@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 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 default_frame(self):
return "plane-elevrev"
def apply_defaultfile_parameters(self):
# plane passes in a defaults_file 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 arming_test_mission(self):
return os.path.join(testdir, "ArduPlane-Missions", "test_arming.txt")
def takeoff(self, alt=150, alt_max=None, relative=True):
"""Takeoff to altitude."""
if alt_max is None:
alt_max = alt + 30
self.change_mode("FBWA")
2018-08-13 08:07:34 -03:00
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(3, 1600)
self.set_rc(4, 1500)
self.wait_groundspeed(12, 100)
# hit the gas harder now, and give it some more elevator
self.set_rc(2, 1100)
self.set_rc(3, 2000)
# gain a bit of altitude
self.wait_altitude(alt, alt_max, timeout=30, 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.mavproxy.send('switch 4\n')
self.wait_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")
self.mavproxy.send('switch 2\n')
self.wait_mode('RTL')
self.wait_location(self.homeloc,
2018-05-09 00:32:23 -03:00
accuracy=120,
target_altitude=self.homeloc.alt+100,
height_accuracy=20,
timeout=180)
self.progress("RTL Complete")
def fly_LOITER(self, num_circles=4):
"""Loiter where we are."""
self.progress("Testing LOITER for %u turns" % num_circles)
self.mavproxy.send('loiter\n')
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_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.mavproxy.send('mode CIRCLE\n')
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_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.mavproxy.send('switch 6\n')
self.wait_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:
2018-05-09 00:32:23 -03:00
self.set_rc(1, 1500)
raise e
count -= 1
# back to FBWA
self.set_rc(1, 1500)
self.mavproxy.send('switch 4\n')
self.wait_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.mavproxy.send('switch 6\n')
self.wait_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.mavproxy.send('switch 4\n')
self.wait_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")
# self.set_parameter("STALL_PREVENTION", 0)
state_roll_over = "roll-over"
state_stabilize_roll = "stabilize-roll"
state_hold = "hold"
state_roll_back = "roll-back"
state_done = "done"
tstart = self.get_sim_time()
try:
state = state_roll_over
while state != state_done:
m = self.mav.recv_match(type='ATTITUDE',
blocking=True,
timeout=0.1)
now = self.get_sim_time_cached()
if now - tstart > 20:
raise AutoTestTimeoutException("Manuevers not completed")
if m is None:
continue
r = math.degrees(m.roll)
if state == state_roll_over:
target_roll_degrees = 60
if abs(r - target_roll_degrees) < tolerance:
state = state_stabilize_roll
stabilize_start = now
elif state == state_stabilize_roll:
# just give it a little time to sort it self out
if now - stabilize_start > 2:
state = state_hold
hold_start = now
elif state == state_hold:
target_roll_degrees = 60
if now - hold_start > tolerance:
state = state_roll_back
if abs(r - target_roll_degrees) > tolerance:
raise NotAchievedException("Failed to hold attitude")
elif state == state_roll_back:
target_roll_degrees = 0
if abs(r - target_roll_degrees) < tolerance:
state = state_done
else:
raise ValueError("Unknown state %s" % str(state))
m_nav = self.mav.messages['NAV_CONTROLLER_OUTPUT']
self.progress("%s Roll: %f desired=%f set=%f" %
(state, r, m_nav.nav_roll, target_roll_degrees))
time_boot_millis = 0 # FIXME
target_system = 1 # FIXME
target_component = 1 # FIXME
type_mask = 0b10000001 ^ 0xFF # FIXME
# attitude in radians:
q = quaternion.Quaternion([math.radians(target_roll_degrees),
2018-11-22 23:51:58 -04:00
0,
0])
roll_rate_radians = 0.5
pitch_rate_radians = 0
yaw_rate_radians = 0
thrust = 1.0
self.mav.mav.set_attitude_target_send(time_boot_millis,
target_system,
target_component,
type_mask,
q,
roll_rate_radians,
pitch_rate_radians,
yaw_rate_radians,
thrust)
except Exception as e:
self.mavproxy.send('mode FBWA\n')
self.wait_mode('FBWA')
self.set_rc(3, 1700)
raise e
# back to FBWA
self.mavproxy.send('mode FBWA\n')
self.wait_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.mavproxy.send("mode STABILIZE\n")
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_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.mavproxy.send("mode ACRO\n")
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_mode('FBWA')
self.wait_level_flight()
self.mavproxy.send("mode ACRO\n")
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_mode('FBWA')
self.set_rc(3, 1700)
return self.wait_level_flight()
def test_FBWB(self, mode='FBWB'):
"""Fly FBWB or CRUISE mode."""
self.mavproxy.send("mode %s\n" % mode)
self.wait_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.mavproxy.send('mode FBWA\n')
self.wait_mode('FBWA')
if abs(final_alt - initial_alt) > 20:
raise NotAchievedException("Failed to maintain altitude")
return self.wait_level_flight()
2018-08-13 08:07:34 -03:00
def fly_mission(self, filename):
"""Fly a mission from a file."""
self.progress("Flying mission %s" % filename)
self.load_mission(filename)
self.mavproxy.send('switch 1\n') # auto mode
self.wait_mode('AUTO')
self.wait_waypoint(1, 7, max_dist=60)
self.wait_groundspeed(0, 0.5, timeout=60)
self.mavproxy.expect("Auto disarmed")
self.progress("Mission OK")
def fly_do_reposition(self):
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,
0,
0,
0,
0,
2019-08-28 09:38:45 -03:00
int(loc.lat*1e7),
int(loc.lng*1e7),
new_alt, # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT_INT,
)
self.wait_altitude(new_alt-10, new_alt, timeout=30, relative=True)
self.fly_home_land_and_disarm()
2019-10-17 17:33:07 -03:00
def fly_deepstall(self):
# self.fly_deepstall_absolute()
self.fly_deepstall_relative()
def fly_deepstall_absolute(self):
self.start_subtest("DeepStall Relative Absolute")
2019-10-17 17:33:07 -03:00
self.set_parameter("LAND_TYPE", 1)
deepstall_elevator_pwm = 1661
self.set_parameter("LAND_DS_ELEV_PWM", deepstall_elevator_pwm)
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")
self.wait_text("Deepstall: Entry: ", timeout=240)
# assume elevator is on channel 2:
self.wait_servo_channel_value(2, deepstall_elevator_pwm)
self.disarm_wait(timeout=120)
self.progress("Flying home")
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")
self.set_parameter("LAND_TYPE", 1)
deepstall_elevator_pwm = 1661
self.set_parameter("LAND_DS_ELEV_PWM", deepstall_elevator_pwm)
self.load_mission("plane-deepstall-relative-mission.txt")
self.change_mode("AUTO")
self.wait_ready_to_arm()
self.arm_vehicle()
self.progress("Waiting for deepstall messages")
self.wait_text("Deepstall: Entry: ", timeout=240)
# assume elevator is on channel 2:
self.wait_servo_channel_value(2, deepstall_elevator_pwm)
self.disarm_wait(timeout=120)
2019-10-17 17:33:07 -03:00
self.progress("Flying home")
self.takeoff(10)
self.set_parameter("LAND_TYPE", 0)
self.fly_home_land_and_disarm()
def fly_do_change_speed(self):
# the following lines ensure we revert these parameter values
# - DO_CHANGE_AIRSPEED is a permanent vehicle change!
self.set_parameter("TRIM_ARSPD_CM", self.get_parameter("TRIM_ARSPD_CM"))
self.set_parameter("MIN_GNDSPD_CM", self.get_parameter("MIN_GNDSPD_CM"))
self.progress("Takeoff")
self.takeoff(alt=100)
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,
0,
0,
0,
0,
12345, # lat*1e7
12345, # lon*1e7
100 # alt
)
self.delay_sim_time(10)
self.progress("Ensuring initial speed is known and relatively constant")
initial_speed = 21.5;
timeout = 10
tstart = self.get_sim_time()
while True:
if self.get_sim_time_cached() - tstart > timeout:
break
m = self.mav.recv_match(type='VFR_HUD', blocking=True)
self.progress("GroundSpeed: %f want=%f" %
(m.groundspeed, initial_speed))
if abs(initial_speed - m.groundspeed) > 1:
raise NotAchievedException("Initial speed not as expected (want=%f got=%f" % (initial_speed, m.groundspeed))
self.progress("Setting groundspeed")
new_target_groundspeed = initial_speed + 5
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
1, # groundspeed
new_target_groundspeed,
-1, # throttle / no change
0, # absolute values
0,
0,
0)
self.wait_groundspeed(new_target_groundspeed-0.5, new_target_groundspeed+0.5, timeout=40)
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-0.5, new_target_groundspeed+0.5, timeout=40)
self.set_parameter("SIM_WIND_SPD", 0)
self.progress("Setting airspeed")
new_target_airspeed = initial_speed + 5
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_CHANGE_SPEED,
0, # airspeed
new_target_airspeed,
-1, # throttle / no change
0, # absolute values
0,
0,
0)
self.wait_groundspeed(new_target_airspeed-0.5, new_target_airspeed+0.5)
self.progress("Adding some wind, hoping groundspeed increases/decreases")
self.set_parameter("SIM_WIND_SPD", 5)
self.set_parameter("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 = 4
self.progress("groundspeed and airspeed should be different (have=%f want=%f)" % (delta, want_delta))
if delta > want_delta:
break
self.fly_home_land_and_disarm()
def fly_home_land_and_disarm(self):
filename = os.path.join(testdir, "flaps.txt")
self.progress("Using %s to fly home" % filename)
self.load_mission(filename)
self.change_mode("AUTO")
self.mavproxy.send('wp set 7\n')
self.mav.motors_disarmed_wait()
2018-08-13 08:07:34 -03:00
def fly_flaps(self):
"""Test flaps functionality."""
filename = os.path.join(testdir, "flaps.txt")
self.context_push()
ex = None
try:
flaps_ch = 5
servo_ch = 5
self.set_parameter("SERVO%u_FUNCTION" % servo_ch, 3) # flapsauto
self.set_parameter("FLAP_IN_CHANNEL", flaps_ch)
self.set_parameter("LAND_FLAP_PERCNT", 50)
self.set_parameter("LOG_DISARMED", 1)
flaps_ch_min = 1000
flaps_ch_trim = 1500
flaps_ch_max = 2000
self.set_parameter("RC%u_MIN" % flaps_ch, flaps_ch_min)
self.set_parameter("RC%u_MAX" % flaps_ch, flaps_ch_max)
self.set_parameter("RC%u_TRIM" % flaps_ch, flaps_ch_trim)
servo_ch_min = 1200
servo_ch_trim = 1300
servo_ch_max = 1800
self.set_parameter("SERVO%u_MIN" % servo_ch, servo_ch_min)
self.set_parameter("SERVO%u_MAX" % servo_ch, servo_ch_max)
self.set_parameter("SERVO%u_TRIM" % servo_ch, servo_ch_trim)
self.progress("check flaps are not deployed")
2018-08-13 08:07:34 -03:00
self.set_rc(flaps_ch, flaps_ch_min)
self.wait_servo_channel_value(servo_ch, servo_ch_min)
self.progress("deploy the flaps")
2018-08-13 08:07:34 -03:00
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")
2018-08-13 08:07:34 -03:00
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)
2018-08-13 08:07:34 -03:00
self.mavproxy.send('wp set 1\n')
self.mavproxy.send('switch 1\n') # auto mode
self.wait_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
last_mission_current_msg = 0
last_seq = None
2018-08-13 08:07:34 -03:00
while self.armed():
m = self.mav.recv_match(type='MISSION_CURRENT', blocking=True)
time_delta = (self.get_sim_time_cached() -
last_mission_current_msg)
2018-11-22 23:51:58 -04:00
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)" %
2018-11-22 23:51:58 -04:00
(m.seq, str(dist)))
last_mission_current_msg = self.get_sim_time_cached()
last_seq = m.seq
2018-08-13 08:07:34 -03:00
# 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)
2018-08-13 08:07:34 -03:00
# self.mavproxy.send('switch 6\n')
# self.wait_mode('MANUAL')
# self.delay_sim_time(10)
2018-08-13 08:07:34 -03:00
self.progress("Flaps OK")
except Exception as e:
ex = e
self.context_pop()
if ex:
if self.armed():
self.disarm_vehicle()
2018-08-13 08:07:34 -03:00
raise ex
def test_rc_relay(self):
'''test toggling channel 12 toggles relay'''
self.set_parameter("RC12_OPTION", 28) # Relay On/Off
self.set_rc(12, 1000)
self.reboot_sitl() # needed for RC12_OPTION 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 test_rc_option_camera_trigger(self):
'''test toggling channel 12 takes picture'''
self.set_parameter("RC12_OPTION", 9) # CameraTrigger
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")
def test_throttle_failsafe(self):
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.set_parameter("SIM_RC_FAIL", 2) # throttle-to-950
self.wait_mode('CIRCLE') # short failsafe
self.wait_mode('RTL') # long failsafe
self.progress("Ensure we've had our throttle squashed to 950")
self.wait_rc_channel_value(3, 950)
self.drain_mav_unparsed()
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
print("%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)
self.drain_mav_unparsed()
# have to allow time for RC to be fetched from SITL
self.delay_sim_time(0.5)
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
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.set_parameter("SIM_RC_FAIL", 1) # no-pulses
self.wait_mode('CIRCLE') # short failsafe
self.wait_mode('RTL') # long failsafe
self.drain_mav_unparsed()
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
print("%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.drain_mav_unparsed()
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
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()
ex = None
try:
self.set_parameter("FS_SHORT_ACTN", 3) # 3 means disabled
self.set_parameter("SIM_RC_FAIL", 1)
self.wait_statustext("Long event on")
self.wait_mode("RTL")
self.set_parameter("SIM_RC_FAIL", 0)
self.wait_text("Long event off")
self.change_mode("MANUAL")
self.progress("Trying again with THR_FS_VALUE")
self.set_parameter("THR_FS_VALUE", 960)
self.set_parameter("SIM_RC_FAIL", 2)
self.wait_statustext("Long event on")
self.wait_mode("RTL")
except Exception as e:
self.progress("Exception caught:")
self.progress(self.get_exception_stacktrace(e))
ex = e
self.context_pop()
if ex is not None:
raise ex
def test_throttle_failsafe_fence(self):
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)
print("%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("FENCE_CHANNEL", 7)
self.set_parameter("FENCE_ACTION", 4)
self.set_rc(3, 1000)
self.set_rc(7, 2000)
self.progress("Checking fence is initially OK")
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
print("%s" % str(m))
if (not (m.onboard_control_sensors_enabled & fence_bit)):
raise NotAchievedException("Fence not initially enabled")
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.drain_mav_unparsed()
self.progress("Checking fence is OK after receiver failure (bind-values)")
fence_bit = mavutil.mavlink.MAV_SYS_STATUS_GEOFENCE
m = self.mav.recv_match(type='SYS_STATUS', blocking=True)
print("%s" % str(m))
if (not (m.onboard_control_sensors_enabled & fence_bit)):
raise NotAchievedException("Fence not enabled after RC fail")
def test_gripper_mission(self):
self.context_push()
ex = None
try:
self.load_mission("plane-gripper-mission.txt")
2018-10-23 01:57:10 -03:00
self.mavproxy.send("wp set 1\n")
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.mavproxy.expect("Gripper Grabbed")
self.mavproxy.expect("Gripper Released")
self.mavproxy.expect("Auto disarmed")
except Exception as e:
self.progress("Exception caught:")
self.progress(self.get_exception_stacktrace(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.drain_mav_unparsed()
m = self.mav.recv_match(type='SYS_STATUS', blocking=True, timeout=1)
if m is None:
raise NotAchievedException("Did not receive SYS_STATUS")
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 do_fence_en_or_dis_able(self, value, want_result=mavutil.mavlink.MAV_RESULT_ACCEPTED):
if value:
p1 = 1
else:
p1 = 0
self.run_cmd(mavutil.mavlink.MAV_CMD_DO_FENCE_ENABLE,
p1, # param1
0, # param2
0, # param3
0, # param4
0, # param5
0, # param6
0, # param7
want_result=want_result)
def do_fence_enable(self, want_result=mavutil.mavlink.MAV_RESULT_ACCEPTED):
self.do_fence_en_or_dis_able(True, want_result=want_result)
def do_fence_disable(self, want_result=mavutil.mavlink.MAV_RESULT_ACCEPTED):
self.do_fence_en_or_dis_able(False, want_result=want_result)
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 test_fence_static(self):
ex = None
try:
self.progress("Checking for bizarre healthy-when-not-present-or-enabled")
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.drain_mav_unparsed()
self.set_parameter("FENCE_ACTION", mavutil.mavlink.FENCE_ACTION_NONE) # report only
self.assert_fence_sys_status(False, False, True)
self.set_parameter("FENCE_ACTION", mavutil.mavlink.FENCE_ACTION_RTL) # report only
self.assert_fence_sys_status(True, False, True)
self.mavproxy.send('fence enable\n')
self.mavproxy.expect("fence enabled")
self.assert_fence_sys_status(True, True, True)
m = self.mav.recv_match(type='FENCE_STATUS', blocking=True, timeout=2)
if m is None:
raise NotAchievedException("Did not get FENCE_STATUS");
if m.breach_status:
raise NotAchievedException("Breached fence unexpectedly (%u)" %
(m.breach_status))
self.mavproxy.send('fence disable\n')
self.mavproxy.expect("fence disabled")
self.assert_fence_sys_status(True, False, True)
self.set_parameter("FENCE_ACTION", mavutil.mavlink.FENCE_ACTION_NONE)
self.assert_fence_sys_status(False, False, True)
self.set_parameter("FENCE_ACTION", mavutil.mavlink.FENCE_ACTION_RTL)
self.assert_fence_sys_status(True, False, True)
self.mavproxy.send("fence clear\n")
self.mavproxy.expect("fence removed")
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", mavutil.mavlink.FENCE_ACTION_RTL)
self.do_fence_enable()
self.assert_fence_sys_status(True, True, True)
self.mavproxy.send("fence clear\n")
self.mavproxy.expect("fence removed")
if self.get_parameter("FENCE_TOTAL") != 0:
raise NotAchievedException("Expected zero points remaining")
self.assert_fence_sys_status(False, False, True)
except Exception as e:
self.progress("Exception caught:")
self.progress(self.get_exception_stacktrace(e))
ex = e
self.mavproxy.send('fence clear\n')
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_parameter("RTL_RADIUS", want_radius)
self.set_parameter("NAVL1_LIM_BANK", 60)
self.set_parameter("FENCE_ACTION", mavutil.mavlink.FENCE_ACTION_RTL)
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.mav.recv_match(type='FENCE_STATUS', blocking=True, timeout=2)
if m is None:
raise NotAchievedException("Did not get FENCE_STATUS");
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.progress("Exception caught:")
self.progress(self.get_exception_stacktrace(e))
ex = e
self.mavproxy.send('fence clear\n')
if ex is not None:
raise ex
def test_fence_rtl(self):
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 test_fence_rtl_rally(self):
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_position_as_mav_location()
self.location_offset_ne(loc, 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)
self.mavproxy.send("rally list\n")
self.test_fence_breach_circle_at(loc)
except Exception as e:
self.progress("Exception caught:")
self.progress(self.get_exception_stacktrace(e))
ex = e
self.mavproxy.send('rally clear\n')
if ex is not None:
raise ex
def test_parachute(self):
self.set_rc(9, 1000)
self.set_parameter("CHUTE_ENABLED", 1)
self.set_parameter("CHUTE_TYPE", 10)
self.set_parameter("SERVO9_FUNCTION", 27)
self.set_parameter("SIM_PARA_ENABLE", 1)
self.set_parameter("SIM_PARA_PIN", 9)
self.load_mission("plane-parachute-mission.txt")
self.mavproxy.send("wp set 1\n")
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.mavproxy.expect("BANG")
self.disarm_vehicle(force=True)
self.reboot_sitl()
def test_parachute_sinkrate(self):
self.set_rc(9, 1000)
self.set_parameter("CHUTE_ENABLED", 1)
self.set_parameter("CHUTE_TYPE", 10)
self.set_parameter("SERVO9_FUNCTION", 27)
self.set_parameter("SIM_PARA_ENABLE", 1)
self.set_parameter("SIM_PARA_PIN", 9)
self.set_parameter("CHUTE_CRT_SINK", 9)
self.progress("Takeoff")
self.takeoff(alt=300)
self.progress("Diving")
self.set_rc(2, 2000)
self.mavproxy.expect("BANG")
self.disarm_vehicle(force=True)
self.reboot_sitl()
def run_subtest(self, desc, func):
self.start_subtest(desc)
func()
def test_main_flight(self):
self.change_mode('MANUAL')
# grab home position:
self.mav.recv_match(type='HOME_POSITION', blocking=True)
self.homeloc = self.mav.location()
self.run_subtest("Takeoff", self.takeoff)
2018-08-13 08:07:34 -03:00
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("Mission test",
lambda: self.fly_mission(
os.path.join(testdir, "ap1.txt")))
def airspeed_autocal(self):
self.progress("Ensure no AIRSPEED_AUTOCAL on ground")
self.set_parameter("ARSPD_AUTOCAL", 1)
m = self.mav.recv_match(type='AIRSPEED_AUTOCAL',
blocking=True,
timeout=5)
if m is not None:
raise NotAchievedException("Got autocal on ground")
mission_filepath = os.path.join(testdir, "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")
m = self.mav.recv_match(type='AIRSPEED_AUTOCAL',
blocking=True,
timeout=5)
self.mav.motors_disarmed_wait()
def test_rangefinder(self):
ex = None
self.context_push()
self.progress("Making sure we don't ordinarily get RANGEFINDER")
m = None
try:
m = self.mav.recv_match(type='RANGEFINDER',
blocking=True,
timeout=5)
except Exception as e:
self.progress("Caught exception: %s" %
self.get_exception_stacktrace(e))
if m is not None:
raise NotAchievedException("Received unexpected RANGEFINDER msg")
try:
self.set_analog_rangefinder_parameters()
self.reboot_sitl()
'''ensure rangefinder gives height-above-ground'''
self.load_mission("plane-gripper-mission.txt") # borrow this
self.mavproxy.send("wp set 1\n")
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.mavproxy.expect("Auto disarmed")
self.progress("Ensure RFND messages in log")
if not self.current_onboard_log_contains_message("RFND"):
raise NotAchievedException("No RFND messages in log")
except Exception as e:
self.progress("Exception caught:")
self.progress(self.get_exception_stacktrace(e))
ex = e
self.context_pop()
self.reboot_sitl()
if ex is not None:
raise ex
def rc_defaults(self):
ret = super(AutoTestPlane, self).rc_defaults()
ret[3] = 1000
ret[8] = 1800
return ret
def default_mode(self):
return "MANUAL"
2019-02-28 19:04:23 -04:00
def test_pid_tuning(self):
self.change_mode("FBWA") # we don't update PIDs in MANUAL
super(AutoTestPlane, self).test_pid_tuning()
def test_setting_modes_via_auxswitches(self):
self.set_parameter("FLTMODE5", 1)
self.mavproxy.send('switch 1\n') # random mode
self.wait_heartbeat()
self.change_mode('MANUAL')
self.mavproxy.send('switch 5\n') # acro mode
self.wait_mode("CIRCLE")
self.set_rc(9, 1000)
self.set_rc(10, 1000)
self.set_parameter("RC9_OPTION", 4) # RTL
self.set_parameter("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 test_adsb_send_threatening_adsb_message(self, here):
self.progress("Sending ABSD_VEHICLE message")
self.mav.mav.adsb_vehicle_send(37, # ICAO address
2019-08-28 09:38:45 -03:00
int(here.lat * 1e7),
int(here.lng * 1e7),
mavutil.mavlink.ADSB_ALTITUDE_TYPE_PRESSURE_QNH,
2019-08-28 09:38:45 -03:00
int(here.alt*1000 + 10000), # 10m up
0, # heading in cdeg
0, # horizontal velocity cm/s
0, # vertical velocity cm/s
2019-08-28 09:38:45 -03:00
"bob".encode("ascii"), # callsign
mavutil.mavlink.ADSB_EMITTER_TYPE_LIGHT,
1, # time since last communication
65535, # flags
17 # squawk
)
def test_adsb(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_parameter("ADSB_ENABLE", 1)
self.set_parameter("AVD_ENABLE", 1)
self.set_parameter("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.mav.recv_match(type='COLLISION', blocking=True, timeout=4)
if m is None:
raise NotAchievedException("Did not get collision message")
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)
print("Got (%s)" % str(m))
if m is not None:
raise NotAchievedException("Got collision message when I shouldn't have")
except Exception as e:
ex = e
self.context_pop()
self.reboot_sitl()
if ex is not None:
raise ex
def fly_do_guided_request(self, target_system=1, target_component=1):
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.mav.recv_match(type='MISSION_ACK', blocking=True, timeout=5)
if m is None:
raise NotAchievedException("Did not get MISSION_ACK")
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.mav.recv_match(type='MISSION_ACK', blocking=True, timeout=5)
if m is None:
raise NotAchievedException("Did not get MISSION_ACK")
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.delay_sim_time(20)
self.wait_altitude(alt_min=desired_relative_alt-3,
alt_max=desired_relative_alt+3,
relative=True)
self.fly_home_land_and_disarm()
def tests(self):
'''return list of all tests'''
ret = super(AutoTestPlane, self).tests()
ret.extend([
("AuxModeSwitch",
"Set modes via auxswitches",
self.test_setting_modes_via_auxswitches),
("TestRCCamera",
"Test RC Option - Camera Trigger",
self.test_rc_option_camera_trigger),
("TestRCRelay", "Test Relay RC Channel Option", self.test_rc_relay),
("ThrottleFailsafe",
"Fly throttle failsafe",
self.test_throttle_failsafe),
("ThrottleFailsafeFence",
"Fly fence survives throttle failsafe",
self.test_throttle_failsafe_fence),
("TestFlaps", "Flaps", self.fly_flaps),
("DO_CHANGE_SPEED", "Test mavlink DO_CHANGE_SPEED command", self.fly_do_change_speed),
("DO_REPOSITION",
"Test mavlink DO_REPOSITION command",
self.fly_do_reposition),
("GuidedRequest",
"Test handling of MISSION_ITEM in guided mode",
self.fly_do_guided_request),
("MainFlight",
"Lots of things in one flight",
self.test_main_flight),
("TestGripperMission",
"Test Gripper mission items",
self.test_gripper_mission),
("Parachute", "Test Parachute", self.test_parachute),
("ParachuteSinkRate", "Test Parachute (SinkRate triggering)", self.test_parachute_sinkrate),
("AIRSPEED_AUTOCAL", "Test AIRSPEED_AUTOCAL", self.airspeed_autocal),
("RangeFinder",
"Test RangeFinder Basic Functionality",
self.test_rangefinder),
("FenceStatic",
"Test Basic Fence Functionality",
self.test_fence_static),
("FenceRTL",
"Test Fence RTL",
self.test_fence_rtl),
("FenceRTLRally",
"Test Fence RTL Rally",
self.test_fence_rtl_rally),
("ADSB",
"Test ADSB",
self.test_adsb),
("Button",
"Test Buttons",
self.test_button),
("AdvancedFailsafe",
"Test Advanced Failsafe",
self.test_advanced_failsafe),
2019-10-17 17:33:07 -03:00
("DeepStall",
"Test DeepStall Landing",
self.fly_deepstall),
("LogDownLoad",
"Log download",
lambda: self.log_download(
self.buildlogs_path("ArduPlane-log.bin"),
timeout=450,
upload_logs=True))
])
return ret