mirror of https://github.com/ArduPilot/ardupilot
951 lines
36 KiB
Python
951 lines
36 KiB
Python
'''
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Fly ArduPlane QuadPlane in SITL
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AP_FLAKE8_CLEAN
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'''
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from __future__ import print_function
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import os
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import numpy
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import math
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from pymavlink import mavutil
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from common import AutoTest
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from common import AutoTestTimeoutException, NotAchievedException, PreconditionFailedException
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import operator
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# get location of scripts
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testdir = os.path.dirname(os.path.realpath(__file__))
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WIND = "0,180,0.2" # speed,direction,variance
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SITL_START_LOCATION = mavutil.location(-27.274439, 151.290064, 343, 8.7)
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class AutoTestQuadPlane(AutoTest):
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@staticmethod
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def get_not_armable_mode_list():
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return []
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@staticmethod
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def get_not_disarmed_settable_modes_list():
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return []
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@staticmethod
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def get_no_position_not_settable_modes_list():
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return []
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@staticmethod
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def get_position_armable_modes_list():
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return []
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@staticmethod
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def get_normal_armable_modes_list():
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return []
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def vehicleinfo_key(self):
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return 'ArduPlane'
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def default_frame(self):
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return "quadplane"
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def test_filepath(self):
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return os.path.realpath(__file__)
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def sitl_start_location(self):
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return SITL_START_LOCATION
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def default_speedup(self):
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'''QuadPlane seems to be race-free'''
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return 100
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def log_name(self):
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return "QuadPlane"
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def set_current_test_name(self, name):
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self.current_test_name_directory = "ArduPlane_Tests/" + name + "/"
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def apply_defaultfile_parameters(self):
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# plane passes in a defaults_filepath in place of applying
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# parameters afterwards.
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pass
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def defaults_filepath(self):
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return self.model_defaults_filepath(self.frame)
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def is_plane(self):
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return True
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def get_stick_arming_channel(self):
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return int(self.get_parameter("RCMAP_YAW"))
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def get_disarm_delay(self):
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return int(self.get_parameter("LAND_DISARMDELAY"))
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def set_autodisarm_delay(self, delay):
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self.set_parameter("LAND_DISARMDELAY", delay)
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def AirMode(self):
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"""Check that plane.air_mode turns on and off as required"""
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self.progress("########## Testing AirMode operation")
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self.set_parameter("AHRS_EKF_TYPE", 10)
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self.change_mode('QSTABILIZE')
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self.wait_ready_to_arm()
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"""
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SPIN_ARM and SPIN_MIN default to 0.10 and 0.15
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when armed with zero throttle in AirMode, motor PWM should be at SPIN_MIN
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If AirMode is off, motor PWM will drop to SPIN_ARM
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"""
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self.progress("Verify that SERVO5 is Motor1 (default)")
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motor1_servo_function_lp = 33
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if (self.get_parameter('SERVO5_FUNCTION') != motor1_servo_function_lp):
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raise PreconditionFailedException("SERVO5_FUNCTION not %d" % motor1_servo_function_lp)
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self.progress("Verify that flightmode channel is 5 (default)")
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default_fltmode_ch = 5
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if (self.get_parameter("FLTMODE_CH") != default_fltmode_ch):
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raise PreconditionFailedException("FLTMODE_CH not %d" % default_fltmode_ch)
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"""When disarmed, motor PWM will drop to min_pwm"""
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min_pwm = self.get_parameter("Q_M_PWM_MIN")
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self.progress("Verify Motor1 is at min_pwm when disarmed")
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self.wait_servo_channel_value(5, min_pwm, comparator=operator.eq)
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armdisarm_option = 154
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arm_ch = 8
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self.set_parameter("RC%d_OPTION" % arm_ch, armdisarm_option)
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self.progress("Configured RC%d as ARMDISARM switch" % arm_ch)
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"""arm with GCS, record Motor1 SPIN_ARM PWM output and disarm"""
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spool_delay = self.get_parameter("Q_M_SPOOL_TIME") + 0.25
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self.zero_throttle()
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self.arm_vehicle()
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self.progress("Waiting for Motor1 to spool up to SPIN_ARM")
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self.delay_sim_time(spool_delay)
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spin_arm_pwm = self.wait_servo_channel_value(5, min_pwm, comparator=operator.gt)
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self.progress("spin_arm_pwm: %d" % spin_arm_pwm)
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self.disarm_vehicle()
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"""arm with switch, record Motor1 SPIN_MIN PWM output and disarm"""
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self.set_rc(8, 2000)
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self.delay_sim_time(spool_delay)
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self.progress("Waiting for Motor1 to spool up to SPIN_MIN")
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spin_min_pwm = self.wait_servo_channel_value(5, spin_arm_pwm, comparator=operator.gt)
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self.progress("spin_min_pwm: %d" % spin_min_pwm)
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self.set_rc(8, 1000)
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if (spin_arm_pwm >= spin_min_pwm):
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raise PreconditionFailedException("SPIN_MIN pwm not greater than SPIN_ARM pwm")
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self.start_subtest("Test auxswitch arming with AirMode Switch")
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for mode in ('QSTABILIZE', 'QACRO'):
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"""verify that arming with switch results in higher PWM output"""
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self.progress("Testing %s mode" % mode)
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self.change_mode(mode)
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self.zero_throttle()
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self.progress("Arming with switch at zero throttle")
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self.arm_motors_with_switch(arm_ch)
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self.progress("Waiting for Motor1 to speed up")
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self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
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self.progress("Verify that rudder disarm is disabled")
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try:
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self.disarm_motors_with_rc_input()
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except NotAchievedException:
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pass
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if not self.armed():
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raise NotAchievedException("Rudder disarm not disabled")
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self.progress("Disarming with switch")
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self.disarm_motors_with_switch(arm_ch)
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self.progress("Waiting for Motor1 to stop")
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self.wait_servo_channel_value(5, min_pwm, comparator=operator.le)
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self.wait_ready_to_arm()
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self.start_subtest("Verify that arming with switch does not spin motors in other modes")
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# introduce a large attitude error to verify that stabilization is not active
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ahrs_trim_x = self.get_parameter("AHRS_TRIM_X")
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self.set_parameter("AHRS_TRIM_X", math.radians(-60))
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self.wait_roll(60, 1)
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# test all modes except QSTABILIZE, QACRO, AUTO and QAUTOTUNE and QLAND and QRTL
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# QRTL and QLAND aren't tested because we can't arm in that mode
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for mode in (
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'ACRO',
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'AUTOTUNE',
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'AVOID_ADSB',
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'CIRCLE',
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'CRUISE',
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'FBWA',
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'FBWB',
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'GUIDED',
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'LOITER',
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'QHOVER',
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'QLOITER',
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'STABILIZE',
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'TRAINING',
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):
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self.progress("Testing %s mode" % mode)
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self.change_mode(mode)
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self.zero_throttle()
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self.progress("Arming with switch at zero throttle")
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self.arm_motors_with_switch(arm_ch)
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self.progress("Waiting for Motor1 to (not) speed up")
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self.delay_sim_time(spool_delay)
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self.wait_servo_channel_value(5, spin_arm_pwm, comparator=operator.le)
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self.wait_servo_channel_value(6, spin_arm_pwm, comparator=operator.le)
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self.wait_servo_channel_value(7, spin_arm_pwm, comparator=operator.le)
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self.wait_servo_channel_value(8, spin_arm_pwm, comparator=operator.le)
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self.progress("Disarming with switch")
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self.disarm_motors_with_switch(arm_ch)
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self.progress("Waiting for Motor1 to stop")
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self.wait_servo_channel_value(5, min_pwm, comparator=operator.le)
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self.wait_ready_to_arm()
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# remove attitude error
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self.set_parameter("AHRS_TRIM_X", ahrs_trim_x)
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self.start_subtest("verify that AIRMODE auxswitch turns airmode on/off while armed")
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"""set RC7_OPTION to AIRMODE"""
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option_airmode = 84
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self.set_parameter("RC7_OPTION", option_airmode)
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for mode in ('QSTABILIZE', 'QACRO'):
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self.progress("Testing %s mode" % mode)
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self.change_mode(mode)
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self.zero_throttle()
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self.progress("Arming with GCS at zero throttle")
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self.arm_vehicle()
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self.progress("Turn airmode on with auxswitch")
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self.set_rc(7, 2000)
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self.progress("Waiting for Motor1 to speed up")
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self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
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self.progress("Turn airmode off with auxswitch")
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self.set_rc(7, 1000)
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self.progress("Waiting for Motor1 to slow down")
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self.wait_servo_channel_value(5, spin_arm_pwm, comparator=operator.le)
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self.disarm_vehicle()
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self.wait_ready_to_arm()
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self.start_subtest("Test GCS arming")
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for mode in ('QSTABILIZE', 'QACRO'):
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self.progress("Testing %s mode" % mode)
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self.change_mode(mode)
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self.zero_throttle()
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self.progress("Arming with GCS at zero throttle")
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self.arm_vehicle()
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self.progress("Turn airmode on with auxswitch")
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self.set_rc(7, 2000)
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self.progress("Waiting for Motor1 to speed up")
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self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
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self.disarm_vehicle_expect_fail()
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self.arm_vehicle()
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self.progress("Verify that airmode is still on")
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self.wait_servo_channel_value(5, spin_min_pwm, comparator=operator.ge)
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self.disarm_vehicle(force=True)
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self.wait_ready_to_arm()
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def TestMotorMask(self):
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"""Check operation of output_motor_mask"""
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"""copter tailsitters will add condition: or (int(self.get_parameter('Q_TAILSIT_MOTMX')) & 1)"""
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if not (int(self.get_parameter('Q_TILT_MASK')) & 1):
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self.progress("output_motor_mask not in use")
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return
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self.progress("Testing output_motor_mask")
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self.wait_ready_to_arm()
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"""Default channel for Motor1 is 5"""
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self.progress('Assert that SERVO5 is Motor1')
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assert 33 == self.get_parameter('SERVO5_FUNCTION')
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modes = ('MANUAL', 'FBWA', 'QHOVER')
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for mode in modes:
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self.progress("Testing %s mode" % mode)
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self.change_mode(mode)
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self.arm_vehicle()
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self.progress("Raising throttle")
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self.set_rc(3, 1800)
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self.progress("Waiting for Motor1 to start")
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self.wait_servo_channel_value(5, 1100, comparator=operator.gt)
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self.set_rc(3, 1000)
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self.disarm_vehicle()
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self.wait_ready_to_arm()
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def fly_mission(self, filename, fence=None, height_accuracy=-1, include_terrain_timeout=False):
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"""Fly a mission from a file."""
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self.progress("Flying mission %s" % filename)
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self.load_mission(filename)
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if fence is not None:
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self.load_fence(fence)
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if self.mavproxy is not None:
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self.mavproxy.send('wp list\n')
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self.install_terrain_handlers_context()
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self.wait_ready_to_arm()
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self.arm_vehicle()
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self.change_mode('AUTO')
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self.wait_waypoint(1, 19, max_dist=60, timeout=1200)
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self.wait_disarmed(timeout=120) # give quadplane a long time to land
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# wait for blood sample here
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self.set_current_waypoint(20)
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self.wait_ready_to_arm()
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self.arm_vehicle()
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self.wait_waypoint(20, 34, max_dist=60, timeout=1200)
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self.wait_disarmed(timeout=120) # give quadplane a long time to land
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self.progress("Mission OK")
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def EXTENDED_SYS_STATE_SLT(self):
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self.set_message_rate_hz(mavutil.mavlink.MAVLINK_MSG_ID_EXTENDED_SYS_STATE, 10)
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self.change_mode("QHOVER")
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self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
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mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
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self.change_mode("FBWA")
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self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_FW,
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mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
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self.change_mode("QHOVER")
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self.wait_ready_to_arm()
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self.arm_vehicle()
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# should not change just because we arm:
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self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
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mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
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self.change_mode("MANUAL")
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self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_FW,
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mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
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self.change_mode("QHOVER")
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self.progress("Taking off")
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self.set_rc(3, 1750)
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self.wait_altitude(1, 5, relative=True)
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self.assert_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
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mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
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self.wait_altitude(10, 15, relative=True)
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self.progress("Transitioning to fixed wing")
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self.change_mode("FBWA")
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self.set_rc(3, 1900) # apply spurs
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self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_TRANSITION_TO_FW,
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mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
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self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_FW,
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mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
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self.progress("Transitioning to multicopter")
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self.set_rc(3, 1500) # apply reins
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self.change_mode("QHOVER")
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# for a standard quadplane there is no transition-to-mc stage.
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# tailsitters do have such a state.
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self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
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mavutil.mavlink.MAV_LANDED_STATE_IN_AIR)
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self.change_mode("QLAND")
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self.wait_altitude(0, 2, relative=True, timeout=60)
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self.wait_extended_sys_state(mavutil.mavlink.MAV_VTOL_STATE_MC,
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mavutil.mavlink.MAV_LANDED_STATE_ON_GROUND)
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self.mav.motors_disarmed_wait()
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def EXTENDED_SYS_STATE(self):
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'''Check extended sys state works'''
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self.EXTENDED_SYS_STATE_SLT()
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def fly_qautotune(self):
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self.change_mode("QHOVER")
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self.wait_ready_to_arm()
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self.arm_vehicle()
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self.set_rc(3, 1800)
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self.wait_altitude(30,
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40,
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relative=True,
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timeout=30)
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self.set_rc(3, 1500)
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self.change_mode("QAUTOTUNE")
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tstart = self.get_sim_time()
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sim_time_expected = 5000
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deadline = tstart + sim_time_expected
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while self.get_sim_time_cached() < deadline:
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now = self.get_sim_time_cached()
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m = self.mav.recv_match(type='STATUSTEXT',
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blocking=True,
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timeout=1)
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if m is None:
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continue
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self.progress("STATUSTEXT (%u<%u): %s" % (now, deadline, m.text))
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if "AutoTune: Success" in m.text:
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break
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self.progress("AUTOTUNE OK (%u seconds)" % (now - tstart))
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self.set_rc(3, 1200)
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self.wait_altitude(-5, 1, relative=True, timeout=30)
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while self.get_sim_time_cached() < deadline:
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self.mavproxy.send('disarm\n')
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try:
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self.wait_text("AutoTune: Saved gains for Roll Pitch Yaw", timeout=0.5)
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except AutoTestTimeoutException:
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continue
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break
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self.wait_disarmed()
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def takeoff(self, height, mode):
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"""climb to specified height and set throttle to 1500"""
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self.set_current_waypoint(0, check_afterwards=False)
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self.change_mode(mode)
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self.wait_ready_to_arm()
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self.arm_vehicle()
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self.set_rc(3, 1800)
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self.wait_altitude(height,
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height+5,
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relative=True,
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timeout=30)
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self.set_rc(3, 1500)
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def do_RTL(self):
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self.change_mode("QRTL")
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self.wait_altitude(-5, 1, relative=True, timeout=60)
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self.wait_disarmed()
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self.zero_throttle()
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def fly_home_land_and_disarm(self, timeout=30):
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self.set_parameter("LAND_TYPE", 0)
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filename = "flaps.txt"
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self.progress("Using %s to fly home" % filename)
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self.load_mission(filename)
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self.change_mode("AUTO")
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self.set_current_waypoint(7)
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self.wait_disarmed(timeout=timeout)
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self.set_current_waypoint(0, check_afterwards=False)
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def wait_level_flight(self, accuracy=5, timeout=30):
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"""Wait for level flight."""
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tstart = self.get_sim_time()
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self.progress("Waiting for level flight")
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self.set_rc(1, 1500)
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self.set_rc(2, 1500)
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self.set_rc(4, 1500)
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while self.get_sim_time_cached() < tstart + timeout:
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m = self.mav.recv_match(type='ATTITUDE', blocking=True)
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roll = math.degrees(m.roll)
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pitch = math.degrees(m.pitch)
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self.progress("Roll=%.1f Pitch=%.1f" % (roll, pitch))
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if math.fabs(roll) <= accuracy and math.fabs(pitch) <= accuracy:
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self.progress("Attained level flight")
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return
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raise NotAchievedException("Failed to attain level flight")
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def fly_left_circuit(self):
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"""Fly a left circuit, 200m on a side."""
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self.mavproxy.send('switch 4\n')
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self.change_mode('FBWA')
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self.set_rc(3, 1700)
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self.wait_level_flight()
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self.progress("Flying left circuit")
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# do 4 turns
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for i in range(0, 4):
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|
# 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 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("LIM_ROLL_CD") * 0.01
|
|
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 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 ICEngine(self):
|
|
'''Test ICE Engine support'''
|
|
rc_engine_start_chan = 11
|
|
self.set_parameters({
|
|
'SERVO13_FUNCTION': 67, # ignition
|
|
'SERVO14_FUNCTION': 69, # starter
|
|
'ICE_ENABLE': 1,
|
|
'ICE_START_CHAN': rc_engine_start_chan,
|
|
'ICE_RPM_CHAN': 1,
|
|
'RPM1_TYPE': 10,
|
|
})
|
|
self.reboot_sitl()
|
|
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, 300, 400, 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()
|
|
|
|
def ICEngineMission(self):
|
|
'''Test ICE Engine Mission support'''
|
|
rc_engine_start_chan = 11
|
|
self.set_parameters({
|
|
'SERVO13_FUNCTION': 67, # ignition
|
|
'SERVO14_FUNCTION': 69, # starter
|
|
'ICE_ENABLE': 1,
|
|
'ICE_START_CHAN': rc_engine_start_chan,
|
|
'ICE_RPM_CHAN': 1,
|
|
'RPM1_TYPE': 10,
|
|
})
|
|
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 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 Mission(self):
|
|
'''fly the OBC 2016 mission in Dalby'''
|
|
self.fly_mission(
|
|
"Dalby-OBC2016.txt",
|
|
"Dalby-OBC2016-fence.txt",
|
|
include_terrain_timeout=True
|
|
)
|
|
|
|
def tests(self):
|
|
'''return list of all tests'''
|
|
|
|
ret = super(AutoTestQuadPlane, self).tests()
|
|
ret.extend([
|
|
self.AirMode,
|
|
self.TestMotorMask,
|
|
self.PilotYaw,
|
|
self.ParameterChecks,
|
|
self.LogDownload,
|
|
self.EXTENDED_SYS_STATE,
|
|
self.Mission,
|
|
self.Weathervane,
|
|
self.QAssist,
|
|
self.GyroFFT,
|
|
self.Tailsitter,
|
|
self.ICEngine,
|
|
self.ICEngineMission,
|
|
self.MidAirDisarmDisallowed,
|
|
self.BootInAUTO,
|
|
self.Ship,
|
|
])
|
|
return ret
|