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ardupilot/Tools/autotest/quadplane.py

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'''
Fly ArduPlane QuadPlane in SITL
AP_FLAKE8_CLEAN
'''
from __future__ import print_function
import os
import numpy
import math
from pymavlink import mavutil
from pymavlink.rotmat import Vector3
import vehicle_test_suite
from vehicle_test_suite import Test
from vehicle_test_suite import AutoTestTimeoutException, NotAchievedException, PreconditionFailedException
import operator
# get location of scripts
testdir = os.path.dirname(os.path.realpath(__file__))
WIND = "0,180,0.2" # speed,direction,variance
SITL_START_LOCATION = mavutil.location(-27.274439, 151.290064, 343, 8.7)
class AutoTestQuadPlane(vehicle_test_suite.TestSuite):
@staticmethod
def get_not_armable_mode_list():
return []
@staticmethod
def get_not_disarmed_settable_modes_list():
return []
@staticmethod
def get_no_position_not_settable_modes_list():
return []
@staticmethod
def get_position_armable_modes_list():
return []
@staticmethod
def get_normal_armable_modes_list():
return []
def vehicleinfo_key(self):
return 'ArduPlane'
def default_frame(self):
return "quadplane"
def test_filepath(self):
return os.path.realpath(__file__)
def sitl_start_location(self):
return SITL_START_LOCATION
def default_speedup(self):
'''QuadPlane seems to be race-free'''
return 100
def log_name(self):
return "QuadPlane"
def set_current_test_name(self, name):
self.current_test_name_directory = "ArduPlane_Tests/" + name + "/"
def apply_defaultfile_parameters(self):
# plane passes in a defaults_filepath in place of applying
# parameters afterwards.
pass
def defaults_filepath(self):
return self.model_defaults_filepath(self.frame)
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 AirMode(self):
"""Check that plane.air_mode turns on and off as required"""
self.progress("########## Testing AirMode operation")
self.set_parameter("AHRS_EKF_TYPE", 10)
self.change_mode('QSTABILIZE')
self.wait_ready_to_arm()
"""
SPIN_ARM and SPIN_MIN default to 0.10 and 0.15
when armed with zero throttle in AirMode, motor PWM should be at SPIN_MIN
If AirMode is off, motor PWM will drop to SPIN_ARM
"""
self.progress("Verify that SERVO5 is Motor1 (default)")
motor1_servo_function_lp = 33
if (self.get_parameter('SERVO5_FUNCTION') != motor1_servo_function_lp):
raise PreconditionFailedException("SERVO5_FUNCTION not %d" % motor1_servo_function_lp)
self.progress("Verify that flightmode channel is 5 (default)")
default_fltmode_ch = 5
if (self.get_parameter("FLTMODE_CH") != default_fltmode_ch):
raise PreconditionFailedException("FLTMODE_CH not %d" % default_fltmode_ch)
"""When disarmed, motor PWM will drop to min_pwm"""
min_pwm = self.get_parameter("Q_M_PWM_MIN")
self.progress("Verify Motor1 is at min_pwm when disarmed")
self.wait_servo_channel_value(5, min_pwm, comparator=operator.eq)
armdisarm_option = 154
arm_ch = 8
self.set_parameter("RC%d_OPTION" % arm_ch, armdisarm_option)
self.progress("Configured RC%d as ARMDISARM switch" % arm_ch)
"""arm with GCS, record Motor1 SPIN_ARM PWM output and disarm"""
spool_delay = self.get_parameter("Q_M_SPOOL_TIME") + 0.25
self.zero_throttle()
self.arm_vehicle()
self.progress("Waiting for Motor1 to spool up to SPIN_ARM")
self.delay_sim_time(spool_delay)
spin_arm_pwm = self.wait_servo_channel_value(5, min_pwm, comparator=operator.gt)
self.progress("spin_arm_pwm: %d" % spin_arm_pwm)
self.disarm_vehicle()
"""arm with switch, record Motor1 SPIN_MIN PWM output and disarm"""
self.set_rc(8, 2000)
self.delay_sim_time(spool_delay)
self.progress("Waiting for Motor1 to spool up to SPIN_MIN")
spin_min_pwm = self.wait_servo_channel_value(5, spin_arm_pwm, comparator=operator.gt)
self.progress("spin_min_pwm: %d" % spin_min_pwm)
self.set_rc(8, 1000)
if (spin_arm_pwm >= spin_min_pwm):
raise PreconditionFailedException("SPIN_MIN pwm not greater than SPIN_ARM pwm")
self.start_subtest("Test auxswitch arming with AirMode Switch")
for mode in ('QSTABILIZE', 'QACRO'):
"""verify that arming with switch results in higher PWM output"""
self.progress("Testing %s mode" % mode)
self.change_mode(mode)
self.zero_throttle()
self.progress("Arming with switch at zero throttle")
self.arm_motors_with_switch(arm_ch)
self.progress("Waiting for Motor1 to speed up")
self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
self.progress("Verify that rudder disarm is disabled")
try:
self.disarm_motors_with_rc_input()
except NotAchievedException:
pass
if not self.armed():
raise NotAchievedException("Rudder disarm not disabled")
self.progress("Disarming with switch")
self.disarm_motors_with_switch(arm_ch)
self.progress("Waiting for Motor1 to stop")
self.wait_servo_channel_value(5, min_pwm, comparator=operator.le)
self.wait_ready_to_arm()
self.start_subtest("Verify that arming with switch does not spin motors in other modes")
# disable compass magnetic field arming check that is triggered by the simulated lean of vehicle
# this is required because adjusting the AHRS_TRIM values only affects the IMU and not external compasses
arming_magthresh = self.get_parameter("ARMING_MAGTHRESH")
self.set_parameter("ARMING_MAGTHRESH", 0)
# introduce a large attitude error to verify that stabilization is not active
ahrs_trim_x = self.get_parameter("AHRS_TRIM_X")
self.set_parameter("AHRS_TRIM_X", math.radians(-60))
self.wait_roll(60, 1)
# test all modes except QSTABILIZE, QACRO, AUTO and QAUTOTUNE and QLAND and QRTL
# QRTL and QLAND aren't tested because we can't arm in that mode
for mode in (
'ACRO',
'AUTOTUNE',
'AVOID_ADSB',
'CIRCLE',
'CRUISE',
'FBWA',
'FBWB',
'GUIDED',
'LOITER',
'QHOVER',
'QLOITER',
'STABILIZE',
'TRAINING',
):
self.progress("Testing %s mode" % mode)
self.change_mode(mode)
self.zero_throttle()
self.progress("Arming with switch at zero throttle")
self.arm_motors_with_switch(arm_ch)
self.progress("Waiting for Motor1 to (not) speed up")
self.delay_sim_time(spool_delay)
self.wait_servo_channel_value(5, spin_arm_pwm, comparator=operator.le)
self.wait_servo_channel_value(6, spin_arm_pwm, comparator=operator.le)
self.wait_servo_channel_value(7, spin_arm_pwm, comparator=operator.le)
self.wait_servo_channel_value(8, spin_arm_pwm, comparator=operator.le)
self.progress("Disarming with switch")
self.disarm_motors_with_switch(arm_ch)
self.progress("Waiting for Motor1 to stop")
self.wait_servo_channel_value(5, min_pwm, comparator=operator.le)
self.wait_ready_to_arm()
# remove attitude error and reinstance compass arming check
self.set_parameter("AHRS_TRIM_X", ahrs_trim_x)
self.set_parameter("ARMING_MAGTHRESH", arming_magthresh)
self.start_subtest("verify that AIRMODE auxswitch turns airmode on/off while armed")
"""set RC7_OPTION to AIRMODE"""
option_airmode = 84
self.set_parameter("RC7_OPTION", option_airmode)
for mode in ('QSTABILIZE', 'QACRO'):
self.progress("Testing %s mode" % mode)
self.change_mode(mode)
self.zero_throttle()
self.progress("Arming with GCS at zero throttle")
self.arm_vehicle()
self.progress("Turn airmode on with auxswitch")
self.set_rc(7, 2000)
self.progress("Waiting for Motor1 to speed up")
self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
self.progress("Turn airmode off with auxswitch")
self.set_rc(7, 1000)
self.progress("Waiting for Motor1 to slow down")
self.wait_servo_channel_value(5, spin_arm_pwm, comparator=operator.le)
self.disarm_vehicle()
self.wait_ready_to_arm()
self.start_subtest("Test GCS arming")
for mode in ('QSTABILIZE', 'QACRO'):
self.progress("Testing %s mode" % mode)
self.change_mode(mode)
self.zero_throttle()
self.progress("Arming with GCS at zero throttle")
self.arm_vehicle()
self.progress("Turn airmode on with auxswitch")
self.set_rc(7, 2000)
self.progress("Waiting for Motor1 to speed up")
self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
self.disarm_vehicle_expect_fail()
self.arm_vehicle()
self.progress("Verify that airmode is still on")
self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
self.disarm_vehicle(force=True)
self.wait_ready_to_arm()
def TestMotorMask(self):
"""Check operation of output_motor_mask"""
"""copter tailsitters will add condition: or (int(self.get_parameter('Q_TAILSIT_MOTMX')) & 1)"""
if not (int(self.get_parameter('Q_TILT_MASK')) & 1):
self.progress("output_motor_mask not in use")
return
self.progress("Testing output_motor_mask")
self.wait_ready_to_arm()
"""Default channel for Motor1 is 5"""
self.progress('Assert that SERVO5 is Motor1')
assert 33 == self.get_parameter('SERVO5_FUNCTION')
modes = ('MANUAL', 'FBWA', 'QHOVER')
for mode in modes:
self.progress("Testing %s mode" % mode)
self.change_mode(mode)
self.arm_vehicle()
self.progress("Raising throttle")
self.set_rc(3, 1800)
self.progress("Waiting for Motor1 to start")
self.wait_servo_channel_value(5, 1100, comparator=operator.gt)
self.set_rc(3, 1000)
self.disarm_vehicle()
self.wait_ready_to_arm()
def fly_mission(self, filename, fence=None, height_accuracy=-1):
"""Fly a mission from a file."""
self.progress("Flying mission %s" % filename)
num_wp = self.load_mission(filename)
if self.mavproxy is not None:
self.mavproxy.send('wp list\n')
if fence is not None:
self.load_fence(fence)
if self.mavproxy is not None:
self.mavproxy.send('fence list\n')
# self.install_terrain_handlers_context()
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_waypoint(1, num_wp-1)
self.wait_disarmed(timeout=120) # give quadplane a long time to land
def EXTENDED_SYS_STATE_SLT(self):
self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, 10)
self.change_mode("QHOVER")
self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
self.change_mode("FBWA")
self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_FW,
mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
self.change_mode("QHOVER")
self.wait_ready_to_arm()
self.arm_vehicle()
# should not change just because we arm:
self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
self.change_mode("MANUAL")
self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_FW,
mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
self.change_mode("QHOVER")
self.progress("Taking off")
self.set_rc(3, 1750)
self.wait_altitude(1, 5, relative=True)
self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
self.wait_altitude(10, 15, relative=True)
self.progress("Transitioning to fixed wing")
self.change_mode("FBWA")
self.set_rc(3, 1900) # apply spurs
self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_TRANSITION_TO_FW,
mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_FW,
mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
self.progress("Transitioning to multicopter")
self.set_rc(3, 1500) # apply reins
self.change_mode("QHOVER")
# for a standard quadplane there is no transition-to-mc stage.
# tailsitters do have such a state.
self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
self.change_mode("QLAND")
self.wait_altitude(0, 2, relative=True, timeout=60)
self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND,
timeout=30)
self.mav.motors_disarmed_wait()
def EXTENDED_SYS_STATE(self):
'''Check extended sys state works'''
self.EXTENDED_SYS_STATE_SLT()
def QAUTOTUNE(self):
'''test Plane QAutoTune mode'''
# this is a list of all parameters modified by QAUTOTUNE. Set
# them so that when the context is popped we get the original
# values back:
parameter_values = self.get_parameters([
"Q_A_RAT_RLL_P",
"Q_A_RAT_RLL_I",
"Q_A_RAT_RLL_D",
"Q_A_ANG_RLL_P",
"Q_A_ACCEL_R_MAX",
"Q_A_RAT_PIT_P",
"Q_A_RAT_PIT_I",
"Q_A_RAT_PIT_D",
"Q_A_ANG_PIT_P",
"Q_A_ACCEL_P_MAX",
"Q_A_RAT_YAW_P",
"Q_A_RAT_YAW_I",
"Q_A_RAT_YAW_FLTE",
"Q_A_ANG_YAW_P",
"Q_A_ACCEL_Y_MAX",
])
self.set_parameters(parameter_values)
self.takeoff(15, mode='GUIDED')
self.set_rc(3, 1500)
self.change_mode("QLOITER")
self.change_mode("QAUTOTUNE")
tstart = self.get_sim_time()
self.context_collect('STATUSTEXT')
while True:
now = self.get_sim_time_cached()
if now - tstart > 5000:
raise NotAchievedException("Did not get success message")
try:
self.wait_text("AutoTune: Success", timeout=1, check_context=True)
except AutoTestTimeoutException:
continue
# got success message
break
self.progress("AUTOTUNE OK (%u seconds)" % (now - tstart))
self.context_clear_collection('STATUSTEXT')
self.progress("Landing to save gains")
self.set_rc(3, 1200)
self.wait_speed_vector(
Vector3(float('nan'), float('nan'), 1.4),
timeout=5,
)
self.wait_speed_vector(
Vector3(0.0, 0.0, 0.0),
timeout=20,
)
distance = self.distance_to_home()
if distance > 20:
raise NotAchievedException("wandered from home (distance=%f)" %
(distance,))
self.set_rc(3, 1000)
tstart = self.get_sim_time()
while True:
now = self.get_sim_time_cached()
if now - tstart > 500:
raise NotAchievedException("Did not get success message")
self.send_mavlink_disarm_command()
try:
self.wait_text(
"AutoTune: Saved gains for Roll Pitch Yaw.*",
timeout=0.5,
check_context=True,
regex=True,
)
except AutoTestTimeoutException:
continue
break
self.wait_disarmed()
self.reboot_sitl() # far from home
def takeoff(self, height, mode, timeout=30):
"""climb to specified height and set throttle to 1500"""
self.set_current_waypoint(0, check_afterwards=False)
self.change_mode(mode)
self.wait_ready_to_arm()
self.arm_vehicle()
if mode == 'GUIDED':
self.user_takeoff(alt_min=height, timeout=timeout)
return
self.set_rc(3, 1800)
self.wait_altitude(height,
height+5,
relative=True,
timeout=timeout)
self.set_rc(3, 1500)
def do_RTL(self):
self.change_mode("QRTL")
self.wait_altitude(-5, 1, relative=True, timeout=60)
self.wait_disarmed()
self.zero_throttle()
def fly_home_land_and_disarm(self, timeout=30):
self.context_push()
self.change_mode('LOITER')
self.set_parameter('RTL_AUTOLAND', 2)
filename = "QuadPlaneDalbyRTL.txt"
self.progress("Using %s to fly home" % filename)
self.load_generic_mission(filename)
self.send_cmd_do_set_mode("RTL")
self.wait_mode('AUTO')
self.wait_current_waypoint(4)
self.wait_statustext('Land descend started')
self.wait_statustext('Land final started', timeout=60)
self.wait_disarmed(timeout=timeout)
self.clear_mission(mavutil.mavlink.MAV_MISSION_TYPE_MISSION)
# the following command is accepted, but doesn't actually
# work! Should be able to remove check_afterwards!
self.set_current_waypoint(0, check_afterwards=False)
self.change_mode('MANUAL')
self.context_pop()
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 fly_left_circuit(self):
"""Fly a left circuit, 200m on a side."""
self.mavproxy.send('switch 4\n')
self.change_mode('FBWA')
self.set_rc(3, 1700)
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")
self.change_mode('QHOVER')
self.set_rc(3, 1100)
self.wait_altitude(10, 15,
relative=True,
timeout=60)
self.set_rc(3, 1500)
def hover_and_check_matched_frequency(self, dblevel=-15, minhz=200, maxhz=300, fftLength=32, peakhz=None):
# find a motor peak
self.takeoff(10, mode="QHOVER")
hover_time = 15
tstart = self.get_sim_time()
self.progress("Hovering for %u seconds" % hover_time)
while self.get_sim_time_cached() < tstart + hover_time:
self.mav.recv_match(type='ATTITUDE', blocking=True)
vfr_hud = self.mav.recv_match(type='VFR_HUD', blocking=True)
tend = self.get_sim_time()
self.do_RTL()
psd = self.mavfft_fttd(1, 0, tstart * 1.0e6, tend * 1.0e6)
# batch sampler defaults give 1024 fft and sample rate of 1kz so roughly 1hz/bin
scale = 1000. / 1024.
sminhz = int(minhz * scale)
smaxhz = int(maxhz * scale)
freq = psd["F"][numpy.argmax(psd["X"][sminhz:smaxhz]) + sminhz]
peakdb = numpy.amax(psd["X"][sminhz:smaxhz])
if peakdb < dblevel or (peakhz is not None and abs(freq - peakhz) / peakhz > 0.05):
raise NotAchievedException("No motor peak, found %fHz at %fdB" % (freq, peakdb))
else:
self.progress("motor peak %fHz, thr %f%%, %fdB" % (freq, vfr_hud.throttle, peakdb))
# we have a peak make sure that the FFT detected something close
# logging is at 10Hz
mlog = self.dfreader_for_current_onboard_log()
# accuracy is determined by sample rate and fft length, given our use of quinn we could probably use half of this
freqDelta = 1000. / fftLength
pkAvg = freq
freqs = []
while True:
m = mlog.recv_match(
type='FTN1',
blocking=True,
condition="FTN1.TimeUS>%u and FTN1.TimeUS<%u" % (tstart * 1.0e6, tend * 1.0e6))
if m is None:
break
freqs.append(m.PkAvg)
# peak within resolution of FFT length
pkAvg = numpy.median(numpy.asarray(freqs))
if abs(pkAvg - freq) > freqDelta:
raise NotAchievedException("FFT did not detect a motor peak at %f, found %f, wanted %f" % (dblevel, pkAvg, freq))
return freq
def GyroFFT(self):
"""Use dynamic harmonic notch to control motor noise."""
# basic gyro sample rate test
self.progress("Flying with gyro FFT - Gyro sample rate")
self.context_push()
ex = None
try:
self.set_rc_default()
# magic tridge EKF type that dramatically speeds up the test
self.set_parameters({
"AHRS_EKF_TYPE": 10,
"INS_LOG_BAT_MASK": 3,
"INS_LOG_BAT_OPT": 0,
"INS_GYRO_FILTER": 100,
"LOG_BITMASK": 45054,
"LOG_DISARMED": 0,
"SIM_DRIFT_SPEED": 0,
"SIM_DRIFT_TIME": 0,
# enable a noisy motor peak
"SIM_GYR1_RND": 20,
# enabling FFT will also enable the arming check: self-testing the functionality
"FFT_ENABLE": 1,
"FFT_MINHZ": 80,
"FFT_MAXHZ": 350,
"FFT_SNR_REF": 10,
"FFT_WINDOW_SIZE": 128,
"FFT_WINDOW_OLAP": 0.75,
})
# Step 1: inject a very precise noise peak at 250hz and make sure the in-flight fft
# can detect it really accurately. For a 128 FFT the frequency resolution is 8Hz so
# a 250Hz peak should be detectable within 5%
self.set_parameters({
"SIM_VIB_FREQ_X": 250,
"SIM_VIB_FREQ_Y": 250,
"SIM_VIB_FREQ_Z": 250,
})
self.reboot_sitl()
# find a motor peak
self.hover_and_check_matched_frequency(-15, 100, 350, 128, 250)
# Step 2: inject actual motor noise and use the standard length FFT to track it
self.set_parameters({
"SIM_VIB_MOT_MAX": 350,
"FFT_WINDOW_SIZE": 32,
"FFT_WINDOW_OLAP": 0.5,
})
self.reboot_sitl()
# find a motor peak
freq = self.hover_and_check_matched_frequency(-15, 200, 300, 32)
# Step 3: add a FFT dynamic notch and check that the peak is squashed
self.set_parameters({
"INS_LOG_BAT_OPT": 2,
"INS_HNTCH_ENABLE": 1,
"INS_HNTCH_FREQ": freq,
"INS_HNTCH_REF": 1.0,
"INS_HNTCH_ATT": 50,
"INS_HNTCH_BW": freq/2,
"INS_HNTCH_MODE": 4,
})
self.reboot_sitl()
self.takeoff(10, mode="QHOVER")
hover_time = 15
ignore_bins = 20
self.progress("Hovering for %u seconds" % hover_time)
tstart = self.get_sim_time()
while self.get_sim_time_cached() < tstart + hover_time:
self.mav.recv_match(type='ATTITUDE', blocking=True)
tend = self.get_sim_time()
self.do_RTL()
psd = self.mavfft_fttd(1, 0, tstart * 1.0e6, tend * 1.0e6)
freq = psd["F"][numpy.argmax(psd["X"][ignore_bins:]) + ignore_bins]
peakdB = numpy.amax(psd["X"][ignore_bins:])
if peakdB < -10:
self.progress("No motor peak, %f at %f dB" % (freq, peakdB))
else:
raise NotAchievedException("Detected peak at %f Hz of %.2f dB" % (freq, peakdB))
# Step 4: take off as a copter land as a plane, make sure we track
self.progress("Flying with gyro FFT - vtol to plane")
self.load_mission("quadplane-gyro-mission.txt")
if self.mavproxy is not None:
self.mavproxy.send('wp list\n')
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_waypoint(1, 7, max_dist=60, timeout=1200)
self.wait_disarmed(timeout=120) # give quadplane a long time to land
# prevent update parameters from messing with the settings when we pop the context
self.set_parameter("FFT_ENABLE", 0)
self.reboot_sitl()
except Exception as e:
self.progress("Exception caught: %s" % (
self.get_exception_stacktrace(e)))
ex = e
self.context_pop()
self.reboot_sitl()
if ex is not None:
raise ex
def PIDTuning(self):
'''Test PID Tuning'''
self.change_mode("FBWA") # we don't update PIDs in MANUAL
super(AutoTestQuadPlane, self).PIDTuning()
def ParameterChecks(self):
'''basic parameter checks'''
self.test_parameter_checks_poscontrol("Q_P")
def rc_defaults(self):
ret = super(AutoTestQuadPlane, self).rc_defaults()
ret[3] = 1000
return ret
def default_mode(self):
return "MANUAL"
def disabled_tests(self):
return {
"FRSkyPassThrough": "Currently failing",
"CPUFailsafe": "servo channel values not scaled like ArduPlane",
"GyroFFT": "flapping test",
"ConfigErrorLoop": "failing because RC values not settable",
}
def BootInAUTO(self):
'''Test behaviour when booting in auto'''
self.load_mission("mission.txt")
self.set_parameters({
})
self.set_rc(5, 1000)
self.wait_mode('AUTO')
self.reboot_sitl()
self.wait_ready_to_arm()
self.delay_sim_time(20)
self.assert_current_waypoint(1)
self.arm_vehicle()
self.wait_altitude(9, 11, relative=True) # value from mission file is 10
distance = self.distance_to_home()
# this distance check is very, very loose. At time of writing
# the vehicle actually pitches ~6 degrees on trakeoff,
# wandering over 1m.
if distance > 2:
raise NotAchievedException("wandered from home (distance=%f)" %
(distance,))
self.change_mode('QLAND')
self.wait_disarmed(timeout=60)
def PilotYaw(self):
'''Test pilot yaw in various modes'''
self.takeoff(10, mode="QLOITER")
self.set_parameter("STICK_MIXING", 0)
self.set_rc(4, 1700)
for mode in "QLOITER", "QHOVER":
self.wait_heading(45)
self.wait_heading(90)
self.wait_heading(180)
self.wait_heading(275)
self.set_rc(4, 1500)
self.do_RTL()
def FwdThrInVTOL(self):
'''test use of fwd motor throttle into wind'''
self.set_parameters({"SIM_WIND_SPD": 25, # need very strong wind for this test
"SIM_WIND_DIR": 360,
"Q_WVANE_ENABLE": 1,
"Q_WVANE_GAIN": 1,
"STICK_MIXING": 0,
"Q_FWD_THR_USE": 2,
"SIM_ENGINE_FAIL": 2}) # we want to fail the forward thrust motor only
self.takeoff(10, mode="QLOITER")
self.set_rc(2, 1000)
self.delay_sim_time(10)
# Check that it is using some forward throttle
fwd_thr_pwm = self.get_servo_channel_value(3)
if fwd_thr_pwm < 1150 :
raise NotAchievedException("fwd motor pwm command low, want >= 1150 got %f" % (fwd_thr_pwm))
# check that pitch is on limit
m = self.mav.recv_match(type='ATTITUDE', blocking=True)
pitch = math.degrees(m.pitch)
if abs(pitch + 3.0) > 0.5 :
raise NotAchievedException("pitch should be -3.0 +- 0.5 deg, got %f" % (pitch))
self.set_rc(2, 1500)
self.delay_sim_time(5)
loc1 = self.mav.location()
self.set_parameter("SIM_ENGINE_MUL", 0) # simulate a complete loss of forward motor thrust
self.delay_sim_time(20)
self.change_mode('QLAND')
self.wait_disarmed(timeout=60)
loc2 = self.mav.location()
position_drift = self.get_distance(loc1, loc2)
if position_drift > 5.0 :
raise NotAchievedException("position drift high, want < 5.0 m got %f m" % (position_drift))
def Weathervane(self):
'''test nose-into-wind functionality'''
# We test nose into wind code paths and yaw direction in copter autotest,
# so we shall test the side into wind yaw direction and plane code paths here.
self.set_parameters({"SIM_WIND_SPD": 10,
"SIM_WIND_DIR": 240,
"Q_WVANE_ENABLE": 3, # WVANE_ENABLE = 3 gives direction of side into wind
"Q_WVANE_GAIN": 3,
"STICK_MIXING": 0})
self.takeoff(10, mode="QLOITER")
# Turn aircraft to heading 90 deg
self.set_rc(4, 1700)
self.wait_heading(90)
self.set_rc(4, 1500)
# Now wait for weathervaning to activate and turn side-on to wind at 240 deg therefore heading 150 deg
self.wait_heading(150, accuracy=5, timeout=180)
self.do_RTL()
def CPUFailsafe(self):
'''In lockup Plane should copy RC inputs to RC outputs'''
self.plane_CPUFailsafe()
def QAssist(self):
'''QuadPlane Assist tests'''
# find a motor peak
self.takeoff(10, mode="QHOVER")
self.set_rc(3, 1800)
self.change_mode("FBWA")
# disable stall prevention so roll angle is not limited
self.set_parameter("STALL_PREVENTION", 0)
thr_min_pwm = self.get_parameter("Q_M_PWM_MIN")
lim_roll_deg = self.get_parameter("ROLL_LIMIT_DEG")
self.progress("Waiting for motors to stop (transition completion)")
self.wait_servo_channel_value(5,
thr_min_pwm,
timeout=30,
comparator=operator.eq)
self.delay_sim_time(5)
self.wait_servo_channel_value(5,
thr_min_pwm,
timeout=30,
comparator=operator.eq)
self.progress("Stopping forward motor to kill airspeed below limit")
self.set_rc(3, 1000)
self.progress("Waiting for qassist to kick in")
self.wait_servo_channel_value(5, 1400, timeout=30, comparator=operator.gt)
self.progress("Move forward again, check qassist stops")
self.set_rc(3, 1800)
self.progress("Checking qassist stops")
self.wait_servo_channel_value(5,
thr_min_pwm,
timeout=30,
comparator=operator.eq)
self.set_rc(3, 1300)
self.context_push()
self.progress("Rolling over to %.0f degrees" % -lim_roll_deg)
self.set_rc(1, 1000)
self.wait_roll(-lim_roll_deg, 5)
self.progress("Killing servo outputs to force qassist to help")
self.set_parameter("SERVO1_MIN", 1480)
self.set_parameter("SERVO1_MAX", 1480)
self.set_parameter("SERVO1_TRIM", 1480)
self.progress("Trying to roll over hard the other way")
self.set_rc(1, 2000)
self.progress("Waiting for qassist (angle) to kick in")
self.wait_servo_channel_value(5, 1100, timeout=30, comparator=operator.gt)
self.wait_roll(lim_roll_deg, 5)
self.context_pop()
self.set_rc(1, 1500)
self.set_parameter("Q_RTL_MODE", 1)
self.change_mode("RTL")
self.wait_disarmed(timeout=300)
def LoiterAltQLand(self):
'''test loitering and qland with terrain involved'''
self.LoiterAltQLand_Terrain(
home="LakeGeorgeLookout",
ofs_n=0,
ofs_e=300,
)
# self.LoiterAltQLand_Terrain(
# home="KalaupapaCliffs",
# ofs_n=500,
# ofs_e=500,
# )
self.LoiterAltQLand_Relative()
def LoiterAltQLand_Relative(self):
'''test failsafe where vehicle loiters in fixed-wing mode to a
specific altitude then changes mode to QLAND'''
self.set_parameters({
'BATT_MONITOR': 4, # LoiterAltQLand
'BATT_FS_LOW_ACT': 6, # LoiterAltQLand
})
self.reboot_sitl()
takeoff_alt = 5
self.takeoff(takeoff_alt, mode='QLOITER')
loc = self.mav.location()
self.location_offset_ne(loc, 500, 500)
new_alt = 100
initial_altitude = self.get_altitude(relative=False, timeout=2)
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
0,
1, # reposition flags; 1 means "change to guided"
0,
0,
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-1,
new_alt+1,
timeout=60,
relative=True,
minimum_duration=10)
self.wait_location(loc, timeout=120, accuracy=100)
self.progress("Triggering failsafe")
self.set_parameter('BATT_LOW_VOLT', 50)
self.wait_mode(25) # LoiterAltQLand
self.drain_mav()
m = self.assert_receive_message('POSITION_TARGET_GLOBAL_INT', very_verbose=True)
q_rtl_alt = self.get_parameter('Q_RTL_ALT')
expected_alt = initial_altitude - takeoff_alt + q_rtl_alt
if abs(m.alt - expected_alt) > 20:
raise NotAchievedException("Unexpected altitude; expected=%f got=%f" %
(expected_alt, m.alt))
self.assert_mode('LOITERALTQLAND')
self.wait_mode('QLAND')
alt = self.get_altitude(relative=True)
if abs(alt - q_rtl_alt) > 2:
raise NotAchievedException("qland too late; want=%f got=%f" %
(alt, q_rtl_alt))
self.wait_disarmed(timeout=300)
def LoiterAltQLand_Terrain(self,
home=None,
ofs_n=None,
ofs_e=None,
reposition_alt=100):
'''test failsafe where vehicle loiters in fixed-wing mode to a
specific altitude then changes mode to QLAND'''
self.context_push()
self.install_terrain_handlers_context()
self.set_parameters({
'BATT_MONITOR': 4, # LoiterAltQLand
'BATT_FS_LOW_ACT': 6, # LoiterAltQLand
'TERRAIN_FOLLOW': 1, # enabled in all modes
})
self.customise_SITL_commandline(
["--home", home]
)
takeoff_alt = 5
self.takeoff(takeoff_alt, mode='QLOITER')
loc = self.mav.location()
self.location_offset_ne(loc, ofs_n, ofs_e)
initial_altitude = self.get_altitude(relative=False, timeout=2)
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
0,
1, # reposition flags; 1 means "change to guided"
0,
0,
int(loc.lat * 1e7),
int(loc.lng * 1e7),
reposition_alt, # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT_INT,
)
self.wait_altitude(
reposition_alt-1,
reposition_alt+1,
timeout=60,
relative=True,
minimum_duration=10)
self.wait_location(loc, timeout=500, accuracy=100)
self.progress("Triggering failsafe")
self.set_parameter('BATT_LOW_VOLT', 50)
self.wait_mode(25) # LoiterAltQLand
terrain_alt = self.get_terrain_height(verbose=True)
self.drain_mav()
m = self.assert_receive_message('POSITION_TARGET_GLOBAL_INT', very_verbose=True)
q_rtl_alt = self.get_parameter('Q_RTL_ALT')
expected_alt = terrain_alt + q_rtl_alt
if abs(m.alt - expected_alt) > 20:
raise NotAchievedException("Unexpected altitude; expected=%f got=%f" %
(expected_alt, m.alt))
self.assert_mode('LOITERALTQLAND')
self.wait_mode('QLAND')
alt = initial_altitude + self.get_altitude(relative=True)
if abs(alt - expected_alt) > 10:
raise NotAchievedException("qland too late; want=%f got=%f" %
(expected_alt, alt))
self.wait_disarmed(timeout=300)
self.zero_throttle()
self.reset_SITL_commandline()
self.context_pop()
def GUIDEDToAUTO(self):
'''Test using GUIDED mode for takeoff before shifting to auto'''
self.load_mission("mission.txt")
self.takeoff(30, mode='GUIDED')
# extra checks would go here
self.assert_not_receiving_message('CAMERA_FEEDBACK')
self.change_mode('AUTO')
self.wait_current_waypoint(3)
self.change_mode('QRTL')
self.wait_disarmed(timeout=240)
def Tailsitter(self):
'''tailsitter test'''
self.set_parameter('Q_FRAME_CLASS', 10)
self.set_parameter('Q_ENABLE', 1)
self.set_parameter('Q_TAILSIT_ENABLE', 1)
self.reboot_sitl()
self.wait_ready_to_arm()
value_before = self.get_servo_channel_value(3)
self.progress("Before: %u" % value_before)
self.change_mode('QHOVER')
tstart = self.get_sim_time()
while True:
now = self.get_sim_time_cached()
if now - tstart > 60:
break
value_after = self.get_servo_channel_value(3)
self.progress("After: t=%f output=%u" % ((now - tstart), value_after))
if value_before != value_after:
raise NotAchievedException("Changed throttle output on mode change to QHOVER")
self.disarm_vehicle()
def setup_ICEngine_vehicle(self, start_chan):
'''restarts SITL with an IC Engine setup'''
self.set_parameters({
'ICE_START_CHAN': start_chan,
})
model = "quadplane-ice"
self.customise_SITL_commandline(
[],
model=model,
defaults_filepath=self.model_defaults_filepath(model),
wipe=False,
)
def ICEngine(self):
'''Test ICE Engine support'''
rc_engine_start_chan = 11
self.setup_ICEngine_vehicle(start_chan=rc_engine_start_chan)
self.wait_ready_to_arm()
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.arm_vehicle()
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.context_collect("STATUSTEXT")
self.progress("Setting engine-start RC switch to HIGH")
self.set_rc(rc_engine_start_chan, 2000)
self.wait_statustext("Starting engine", check_context=True)
self.wait_rpm(1, 300, 400, minimum_duration=1)
self.progress("Setting engine-start RC switch to MID")
self.set_rc(rc_engine_start_chan, 1500)
self.progress("Setting full throttle")
self.set_rc(3, 2000)
self.wait_rpm(1, 6500, 7500, minimum_duration=30, timeout=40)
self.progress("Setting min-throttle")
self.set_rc(3, 1000)
self.wait_rpm(1, 65, 75, minimum_duration=1)
self.progress("Setting engine-start RC switch to LOW")
self.set_rc(rc_engine_start_chan, 1000)
self.wait_rpm(1, 0, 0, minimum_duration=1)
# ICE provides forward thrust, which can make us think we're flying:
self.disarm_vehicle(force=True)
self.reboot_sitl()
self.start_subtest("Testing throttle out in manual mode")
self.change_mode('MANUAL')
self.set_rc(3, 1700)
self.wait_servo_channel_value(3, 2000)
self.set_parameter("ICE_OPTIONS", 4)
# remember that throttle is reversed!
self.wait_servo_channel_value(3, 1300)
self.change_mode('FBWA')
self.wait_servo_channel_value(3, 2000)
def ICEngineMission(self):
'''Test ICE Engine Mission support'''
rc_engine_start_chan = 11
self.setup_ICEngine_vehicle(start_chan=rc_engine_start_chan)
self.load_mission("mission.txt")
self.wait_ready_to_arm()
self.set_rc(rc_engine_start_chan, 2000)
self.arm_vehicle()
self.change_mode('AUTO')
self.wait_disarmed(timeout=300)
def MAV_CMD_DO_ENGINE_CONTROL(self):
'''test MAV_CMD_DO_ENGINE_CONTROL mavlink command'''
expected_idle_rpm_min = 65
expected_idle_rpm_max = 75
expected_starter_rpm_min = 345
expected_starter_rpm_max = 355
rc_engine_start_chan = 11
self.setup_ICEngine_vehicle(start_chan=rc_engine_start_chan)
self.wait_ready_to_arm()
for method in self.run_cmd, self.run_cmd_int:
self.change_mode('MANUAL')
self.set_rc(rc_engine_start_chan, 1500) # allow motor to run
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.arm_vehicle()
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.start_subtest("Start motor")
method(mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL, p1=1)
self.wait_rpm(1, expected_starter_rpm_min, expected_starter_rpm_max)
self.wait_rpm(1, expected_idle_rpm_min, expected_idle_rpm_max, minimum_duration=10)
# starting the motor while it is running is failure
# (probably wrong, but that's how this works):
self.start_subtest("try start motor again")
self.context_collect('STATUSTEXT')
method(mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL, p1=1, want_result=mavutil.mavlink.MAV_RESULT_FAILED)
self.wait_statustext("already running", check_context=True)
self.context_stop_collecting('STATUSTEXT')
# shouldn't affect run state:
self.wait_rpm(1, expected_idle_rpm_min, expected_idle_rpm_max, minimum_duration=1)
self.start_subtest("Stop motor")
method(mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL, p1=0)
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.start_subtest("Stop motor (again)")
method(mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL, p1=0)
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.start_subtest("Check start chan control disable")
old_start_channel_value = self.get_rc_channel_value(rc_engine_start_chan)
self.set_rc(rc_engine_start_chan, 1000)
self.context_collect('STATUSTEXT')
method(mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL, p1=1, want_result=mavutil.mavlink.MAV_RESULT_FAILED)
self.wait_statustext("start control disabled", check_context=True)
self.context_stop_collecting('STATUSTEXT')
self.set_rc(rc_engine_start_chan, old_start_channel_value)
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.start_subtest("test start-at-height")
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.context_collect('STATUSTEXT')
method(
mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL,
p1=1, # start
p3=15.5, # ... at 15.5 metres
)
self.wait_statustext("height set to 15.5m", check_context=True)
self.wait_rpm(1, 0, 0, minimum_duration=2)
self.takeoff(20, mode='GUIDED')
self.wait_rpm(1, expected_starter_rpm_min, expected_starter_rpm_max, minimum_duration=1)
self.wait_statustext("Engine running", check_context=True)
self.context_stop_collecting('STATUSTEXT')
# stop the motor again:
method(mavutil.mavlink.MAV_CMD_DO_ENGINE_CONTROL, p1=0)
self.wait_rpm(1, 0, 0, minimum_duration=1)
self.change_mode('QLAND')
self.wait_disarmed()
def Ship(self):
'''Ensure we can take off from simulated ship'''
self.context_push()
self.set_parameters({
'SIM_SHIP_ENABLE': 1,
'SIM_SHIP_SPEED': 1, # the default of 3 will break this test
})
self.change_mode('QLOITER')
self.wait_ready_to_arm()
self.arm_vehicle()
self.set_rc(3, 1700)
# self.delay_sim_time(1)
# self.send_debug_trap()
# output here is a bit weird as we also receive altitude from
# the simulated ship....
self.wait_altitude(20, 30, relative=True)
self.disarm_vehicle(force=True)
self.context_pop()
self.reboot_sitl()
def MidAirDisarmDisallowed(self):
'''Check disarm behaviour in Q-mode'''
self.start_subtest("Basic arm in qloiter")
self.set_parameter("FLIGHT_OPTIONS", 0)
self.change_mode('QLOITER')
self.wait_ready_to_arm()
self.arm_vehicle()
self.disarm_vehicle()
self.context_push()
self.start_subtest("Ensure disarming in q-modes on ground works")
self.set_parameter("FLIGHT_OPTIONS", 1 << 11)
self.arm_vehicle()
self.disarm_vehicle() # should be OK as we're not flying yet
self.context_pop()
self.start_subtest("Ensure no disarming mid-air")
self.arm_vehicle()
self.set_rc(3, 2000)
self.wait_altitude(5, 50, relative=True)
self.set_rc(3, 1000)
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")
self.change_mode('QLAND')
self.wait_disarmed()
self.start_subtest("Check we can disarm after a short period on the ground")
self.takeoff(5, 'QHOVER')
self.change_mode('QLAND')
try:
self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, 10)
self.wait_extended_sys_state(
landed_state=mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND,
vtol_state=mavutil.mavlink.MAV_VTOL_STATE_MC,
timeout=60
)
except Exception:
self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, 0)
raise
self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, -1)
self.disarm_vehicle()
def MAV_CMD_NAV_LOITER_TO_ALT(self, target_system=1, target_component=1):
'''ensure consecutive loiter to alts work'''
self.load_mission('mission.txt')
self.change_mode('AUTO')
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_current_waypoint(4, timeout=240)
self.assert_altitude(120, accuracy=5, relative=True)
self.delay_sim_time(30)
self.assert_altitude(120, accuracy=5, relative=True)
self.set_current_waypoint(5)
self.wait_altitude(altitude_min=65, altitude_max=75, relative=True)
if self.current_waypoint() != 5:
raise NotAchievedException("Should pass 90m before passing waypoint 5")
self.wait_disarmed(timeout=300)
def Mission(self):
'''fly the OBC 2016 mission in Dalby'''
self.load_mission("Dalby-OBC2016.txt")
self.load_fence("Dalby-OBC2016-fence.txt")
if self.mavproxy is not None:
self.mavproxy.send('wp list\n')
self.install_terrain_handlers_context()
self.wait_ready_to_arm()
self.arm_vehicle()
self.change_mode('AUTO')
self.wait_waypoint(1, 19, max_dist=60, timeout=1200)
self.wait_disarmed(timeout=120) # give quadplane a long time to land
# wait for blood sample here
self.set_current_waypoint(20)
self.wait_ready_to_arm()
self.arm_vehicle()
self.wait_waypoint(20, 34, max_dist=60, timeout=1200)
self.wait_disarmed(timeout=120) # give quadplane a long time to land
self.progress("Mission OK")
def VTOLLandSpiral(self):
'''check spiral-to-alt option for landing'''
self.fly_mission('mission.txt')
self.set_parameter('WP_LOITER_RAD', -self.get_parameter('WP_LOITER_RAD'))
self.set_current_waypoint(0, check_afterwards=False)
self.fly_mission('mission.txt')
def VTOLQuicktune(self):
'''VTOL Quicktune'''
applet_script = "VTOL-quicktune.lua"
self.install_applet_script(applet_script)
self.set_parameters({
"SCR_ENABLE": 1,
"SIM_SPEEDUP": 20, # need to give some cycles to lua
"RC7_OPTION": 300,
})
self.reboot_sitl()
self.context_push()
self.context_collect('STATUSTEXT')
self.set_parameters({
"QUIK_ENABLE" : 1,
"QUIK_DOUBLE_TIME" : 5, # run faster for autotest
})
self.scripting_restart()
self.wait_text("Quicktune for quadplane loaded", check_context=True)
self.wait_ready_to_arm()
self.change_mode("QLOITER")
self.arm_vehicle()
self.takeoff(20, 'QLOITER')
# use rc switch to start tune
self.set_rc(7, 1500)
self.wait_text("Tuning: starting tune", check_context=True)
for axis in ['RLL', 'PIT', 'YAW']:
self.wait_text("Starting %s tune" % axis, check_context=True)
self.wait_text("Tuning: %s_D done" % axis, check_context=True, timeout=120)
self.wait_text("Tuning: %s_P done" % axis, check_context=True, timeout=120)
self.wait_text("Tuning: %s done" % axis, check_context=True, timeout=120)
self.wait_text("Tuning: YAW done", check_context=True, timeout=120)
# to test aux function method, use aux fn for save
self.run_auxfunc(300, 2)
self.wait_text("Tuning: saved", check_context=True)
self.change_mode("QLAND")
self.wait_disarmed(timeout=120)
self.set_parameter("QUIK_ENABLE", 0)
self.context_pop()
self.remove_installed_script(applet_script)
self.reboot_sitl()
def RCDisableAirspeedUse(self):
'''check disabling airspeed using RC switch'''
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)
self.progress("Disabling airspeed sensor")
self.context_push()
self.set_rc(9, 2000)
self.set_parameters({
"COMPASS_ENABLE": 0,
"EK2_ENABLE": 0,
"AHRS_EKF_TYPE": 3,
"COMPASS_USE": 0,
"COMPASS_USE2": 0,
"COMPASS_USE3": 0,
"ARMING_CHECK": 589818, # from a logfile, disables compass
})
self.reboot_sitl()
self.context_collect('STATUSTEXT')
self.wait_prearm_sys_status_healthy(timeout=120)
self.change_mode('QLOITER')
self.arm_vehicle()
self.set_rc(3, 2000)
self.wait_altitude(10, 30, relative=True)
self.change_mode('FBWA')
self.wait_statustext('Transition done')
# the vehicle stays in DCM until there's velocity - make sure
# we did go to EK3 evenutally, 'though:
self.wait_statustext('EKF3 active', check_context=True)
self.disarm_vehicle(force=True)
self.context_pop()
self.reboot_sitl()
def mission_MAV_CMD_DO_VTOL_TRANSITION(self):
'''mission item forces transition'''
wps = self.create_simple_relhome_mission([
(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, 0, 0, 30),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 200, 0, 30),
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_DO_VTOL_TRANSITION,
p1=mavutil.mavlink.MAV_VTOL_STATE_MC
),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 300, 200, 30),
self.create_MISSION_ITEM_INT(
mavutil.mavlink.MAV_CMD_DO_VTOL_TRANSITION,
p1=mavutil.mavlink.MAV_VTOL_STATE_FW
),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 100, 200, 30),
(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(4)
self.wait_servo_channel_value(5, 1200, comparator=operator.gt)
self.wait_current_waypoint(6)
self.wait_servo_channel_value(5, 1000, comparator=operator.eq, timeout=90)
self.fly_home_land_and_disarm()
def mavlink_MAV_CMD_DO_VTOL_TRANSITION(self):
'''mavlink command forces transition during mission'''
wps = self.create_simple_relhome_mission([
(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, 0, 0, 30),
(mavutil.mavlink.MAV_CMD_NAV_WAYPOINT, 2000, 0, 30),
(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)
self.wait_servo_channel_value(5, 1000, comparator=operator.eq, timeout=90)
for command in self.run_cmd, self.run_cmd_int:
command(mavutil.mavlink.MAV_CMD_DO_VTOL_TRANSITION, p1=mavutil.mavlink.MAV_VTOL_STATE_MC)
self.wait_servo_channel_value(5, 1200, comparator=operator.gt, timeout=300)
command(mavutil.mavlink.MAV_CMD_DO_VTOL_TRANSITION, p1=mavutil.mavlink.MAV_VTOL_STATE_FW)
self.wait_servo_channel_value(5, 1000, comparator=operator.eq, timeout=90)
self.fly_home_land_and_disarm()
def MAV_CMD_NAV_TAKEOFF(self):
'''test issuing takeoff command via mavlink'''
self.change_mode('GUIDED')
self.wait_ready_to_arm()
self.arm_vehicle()
self.run_cmd(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, p7=5)
self.wait_altitude(4.5, 5.5, minimum_duration=5, relative=True)
self.change_mode('QLAND')
self.wait_disarmed()
self.start_subtest("Check NAV_TAKEOFF is above current location, not home location")
self.change_mode('GUIDED')
self.wait_ready_to_arm()
# reset home 20 metres above current location
current_alt_abs = self.get_altitude(relative=False)
loc = self.mav.location()
home_z_ofs = 20
self.run_cmd(
mavutil.mavlink.MAV_CMD_DO_SET_HOME,
p5=loc.lat,
p6=loc.lng,
p7=current_alt_abs + home_z_ofs,
)
self.arm_vehicle()
takeoff_alt = 5
self.run_cmd(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, p7=takeoff_alt)
self.wait_altitude(
current_alt_abs + takeoff_alt - 0.5,
current_alt_abs + takeoff_alt + 0.5,
minimum_duration=5,
relative=False,
)
self.change_mode('QLAND')
self.wait_disarmed()
self.reboot_sitl() # unlock home position
def Q_GUIDED_MODE(self):
'''test moving in VTOL mode with SET_POSITION_TARGET_GLOBAL_INT'''
self.set_parameter('Q_GUIDED_MODE', 1)
self.change_mode('GUIDED')
self.wait_ready_to_arm()
self.arm_vehicle()
self.run_cmd(mavutil.mavlink.MAV_CMD_NAV_TAKEOFF, p7=15)
self.wait_altitude(14, 16, relative=True)
loc = self.mav.location()
self.location_offset_ne(loc, 50, 50)
# set position target
self.run_cmd_int(
mavutil.mavlink.MAV_CMD_DO_REPOSITION,
0,
1, # reposition flags; 1 means "change to guided"
0,
0,
int(loc.lat * 1e7),
int(loc.lng * 1e7),
30, # alt
frame=mavutil.mavlink.MAV_FRAME_GLOBAL_RELATIVE_ALT_INT,
)
self.wait_location(loc, timeout=120)
self.fly_home_land_and_disarm()
def DCMClimbRate(self):
'''Test the climb rate measurement in DCM with and without GPS'''
self.wait_ready_to_arm()
self.change_mode('QHOVER')
self.arm_vehicle()
self.set_rc(3, 2000)
self.wait_altitude(30, 50, relative=True)
# Start Descending
self.set_rc(3, 1000)
self.wait_climbrate(-5, -0.5, timeout=10)
# Switch to DCM
self.set_parameter('AHRS_EKF_TYPE', 0)
self.delay_sim_time(5)
# Start Climbing
self.set_rc(3, 2000)
self.wait_climbrate(0.5, 5, timeout=10)
# Kill any GPSs
self.set_parameters({
'SIM_GPS_DISABLE': 1,
'SIM_GPS2_DISABLE': 1,
})
self.delay_sim_time(5)
# Start Descending
self.set_rc(3, 1000)
self.wait_climbrate(-5, -0.5, timeout=10)
# Force disarm
self.disarm_vehicle(force=True)
def tests(self):
'''return list of all tests'''
ret = super(AutoTestQuadPlane, self).tests()
ret.extend([
self.FwdThrInVTOL,
self.AirMode,
self.TestMotorMask,
self.PilotYaw,
self.ParameterChecks,
self.QAUTOTUNE,
self.TestLogDownload,
self.TestLogDownloadWrap,
self.EXTENDED_SYS_STATE,
self.Mission,
self.Weathervane,
self.QAssist,
self.GyroFFT,
self.Tailsitter,
self.ICEngine,
self.ICEngineMission,
self.MAV_CMD_DO_ENGINE_CONTROL,
self.MidAirDisarmDisallowed,
self.GUIDEDToAUTO,
self.BootInAUTO,
self.Ship,
self.MAV_CMD_NAV_LOITER_TO_ALT,
self.LoiterAltQLand,
self.VTOLLandSpiral,
self.VTOLQuicktune,
Test(self.MotorTest, kwargs={ # tests motors 4 and 2
"mot1_servo_chan": 8, # quad-x second motor cw from f-r
"mot4_servo_chan": 6, # quad-x third motor cw from f-r
"wait_finish_text": False,
"quadplane": True,
}),
self.RCDisableAirspeedUse,
self.mission_MAV_CMD_DO_VTOL_TRANSITION,
self.mavlink_MAV_CMD_DO_VTOL_TRANSITION,
self.MAV_CMD_NAV_TAKEOFF,
self.Q_GUIDED_MODE,
self.DCMClimbRate,
])
return ret
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