''' Fly ArduPlane QuadPlane in SITL AP_FLAKE8_CLEAN ''' from __future__ import print_function import os import numpy import math from pymavlink import mavutil from common import AutoTest from common 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(AutoTest): @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 test_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") # 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', 'RTL', '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 self.set_parameter("AHRS_TRIM_X", ahrs_trim_x) 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.progress("Disarm/rearm with GCS") self.disarm_vehicle() 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() self.wait_ready_to_arm() def test_motor_mask(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) self.load_mission(filename) if fence is not None: self.load_fence(fence) if self.mavproxy is not None: self.mavproxy.send('wp list\n') 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 enum_state_name(self, enum_name, state, pretrim=None): e = mavutil.mavlink.enums[enum_name] e_value = e[state] name = e_value.name if pretrim is not None: if not pretrim.startswith(pretrim): raise NotAchievedException("Expected %s to pretrim" % (pretrim)) name = name.replace(pretrim, "") return name def vtol_state_name(self, state): return self.enum_state_name("MAV_VTOL_STATE", state, pretrim="MAV_VTOL_STATE_") def landed_state_name(self, state): return self.enum_state_name("MAV_LANDED_STATE", state, pretrim="MAV_LANDED_STATE_") def assert_extended_sys_state(self, vtol_state, landed_state): m = self.assert_receive_message('EXTENDED_SYS_STATE', timeout=1) if m.vtol_state != vtol_state: raise ValueError("Bad MAV_VTOL_STATE. Want=%s got=%s" % (self.vtol_state_name(vtol_state), self.vtol_state_name(m.vtol_state))) if m.landed_state != landed_state: raise ValueError("Bad MAV_LANDED_STATE. Want=%s got=%s" % (self.landed_state_name(landed_state), self.landed_state_name(m.landed_state))) def wait_extended_sys_state(self, vtol_state, landed_state): tstart = self.get_sim_time() while True: if self.get_sim_time() - tstart > 10: raise NotAchievedException("Did not achieve vol/landed states") self.progress("Waiting for MAV_VTOL_STATE=%s MAV_LANDED_STATE=%s" % (self.vtol_state_name(vtol_state), self.landed_state_name(landed_state))) m = self.assert_receive_message('EXTENDED_SYS_STATE', verbose=True) if m.landed_state != landed_state: self.progress("Wrong MAV_LANDED_STATE (want=%s got=%s)" % (self.landed_state_name(landed_state), self.landed_state_name(m.landed_state))) continue if m.vtol_state != vtol_state: self.progress("Wrong MAV_VTOL_STATE (want=%s got=%s)" % (self.vtol_state_name(vtol_state), self.vtol_state_name(m.vtol_state))) continue self.progress("vtol and landed states match") return 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) self.mav.motors_disarmed_wait() def EXTENDED_SYS_STATE(self): self.EXTENDED_SYS_STATE_SLT() def fly_qautotune(self): self.change_mode("QHOVER") self.wait_ready_to_arm() self.arm_vehicle() self.set_rc(3, 1800) self.wait_altitude(30, 40, relative=True, timeout=30) self.set_rc(3, 1500) self.change_mode("QAUTOTUNE") tstart = self.get_sim_time() sim_time_expected = 5000 deadline = tstart + sim_time_expected while self.get_sim_time_cached() < deadline: now = self.get_sim_time_cached() m = self.mav.recv_match(type='STATUSTEXT', blocking=True, timeout=1) if m is None: continue self.progress("STATUSTEXT (%u<%u): %s" % (now, deadline, m.text)) if "AutoTune: Success" in m.text: break self.progress("AUTOTUNE OK (%u seconds)" % (now - tstart)) self.set_rc(3, 1200) self.wait_altitude(-5, 1, relative=True, timeout=30) while self.get_sim_time_cached() < deadline: self.mavproxy.send('disarm\n') try: self.wait_text("AutoTune: Saved gains for Roll Pitch Yaw", timeout=0.5) except AutoTestTimeoutException: continue break self.wait_disarmed() def takeoff(self, height, mode): """climb to specified height and set throttle to 1500""" self.change_mode(mode) self.wait_ready_to_arm() self.arm_vehicle() self.set_rc(3, 1800) self.wait_altitude(height, height+5, relative=True, timeout=30) 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.set_parameter("LAND_TYPE", 0) filename = "flaps.txt" self.progress("Using %s to fly home" % filename) self.load_mission(filename) self.change_mode("AUTO") self.set_current_waypoint(7) self.wait_disarmed(timeout=timeout) 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 fly_gyro_fft(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 test_pid_tuning(self): self.change_mode("FBWA") # we don't update PIDs in MANUAL super(AutoTestQuadPlane, self).test_pid_tuning() def test_parameter_checks(self): 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 test_pilot_yaw(self): 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_test(self): # 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 test_qassist(self): # 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 tests(self): '''return list of all tests''' ret = super(AutoTestQuadPlane, self).tests() ret.extend([ ("TestAirMode", "Test airmode", self.test_airmode), ("TestMotorMask", "Test output_motor_mask", self.test_motor_mask), ("PilotYaw", "Test pilot yaw in various modes", self.test_pilot_yaw), ("ParameterChecks", "Test Arming Parameter Checks", self.test_parameter_checks), ("TestLogDownload", "Test Onboard Log Download", self.test_log_download), ("EXTENDED_SYS_STATE", "Check extended sys state works", self.EXTENDED_SYS_STATE), ("Mission", "Dalby Mission", lambda: self.fly_mission("Dalby-OBC2016.txt", "Dalby-OBC2016-fence.txt")), ("Weathervane", "Test Weathervane Functionality", self.weathervane_test), ("QAssist", "QuadPlane Assist tests", self.test_qassist), ("GyroFFT", "Fly Gyro FFT", self.fly_gyro_fft), ("Tailsitter", "Test tailsitter support", self.tailsitter), ("LogUpload", "Log upload", self.log_upload), ]) return ret