mirror of https://github.com/ArduPilot/ardupilot
autotest: new harmonic notch test
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@ -3657,32 +3657,91 @@ class AutoTestCopter(AutoTest):
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(tdelta, max_good_tdelta))
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self.progress("Vehicle returned")
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def fly_dynamic_notches(self):
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self.progress("Flying with dynamic notches")
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# magic tridge EKF type that dramatically speeds up the test
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self.set_parameter("AHRS_EKF_TYPE", 10)
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self.set_parameter("INS_HNTCH_ENABLE", 1)
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self.set_parameter("INS_HNTCH_FREQ", 80)
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self.set_parameter("INS_HNTCH_REF", 0.35)
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# first and third harmonic
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self.set_parameter("INS_HNTCH_HMNCS", 5)
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self.set_parameter("INS_NOTCH_ENABLE", 1)
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self.set_parameter("INS_NOTCH_FREQ", 90)
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self.reboot_sitl()
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def hover_and_check_matched_frequency_with_fft(self, dblevel=-15, minhz=200, maxhz=300, peakhz=None, reverse=None):
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# find a motor peak
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self.takeoff(10, mode="ALT_HOLD")
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self.set_parameter("SIM_GYR_RND", 10)
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self.takeoff(10, mode="LOITER")
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self.change_mode("ALT_HOLD")
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# fly fast forrest!
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self.set_rc(3, 1900)
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self.set_rc(2, 1200)
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self.wait_groundspeed(5, 1000)
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self.set_rc(3, 1500)
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self.set_rc(2, 1500)
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hover_time = 15
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tstart = self.get_sim_time()
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self.progress("Hovering for %u seconds" % hover_time)
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while self.get_sim_time_cached() < tstart + hover_time:
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attitude = self.mav.recv_match(type='ATTITUDE', blocking=True)
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vfr_hud = self.mav.recv_match(type='VFR_HUD', blocking=True)
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tend = self.get_sim_time()
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self.do_RTL()
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psd = self.mavfft_fttd(1, 0, tstart * 1.0e6, tend * 1.0e6)
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# batch sampler defaults give 1024 fft and sample rate of 1kz so roughly 1hz/bin
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freq = psd["F"][numpy.argmax(psd["X"][minhz:maxhz]) + minhz] * (1000. / 1024.)
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peakdb = numpy.amax(psd["X"][minhz:maxhz])
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if peakdb < dblevel or (peakhz is not None and abs(freq - peakhz) / peakhz > 0.05):
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if reverse is not None:
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self.progress("Did not detect a motor peak, found %fHz at %fdB" % (freq, peakdb))
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else:
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raise NotAchievedException("Did not detect a motor peak, found %fHz at %fdB" % (freq, peakdb))
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else:
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if reverse is not None:
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raise NotAchievedException("Detected motor peak at %fHz, throttle %f%%, %fdB" % (freq, vfr_hud.throttle, peakdb))
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else:
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self.progress("Detected motor peak at %fHz, throttle %f%%, %fdB" % (freq, vfr_hud.throttle, peakdb))
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return freq, vfr_hud, peakdb
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def fly_dynamic_notches(self):
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"""Use dynamic harmonic notch to control motor noise."""
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self.progress("Flying with dynamic notches")
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self.context_push()
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ex = None
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try:
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self.set_rc_default()
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self.set_parameter("AHRS_EKF_TYPE", 10)
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self.set_parameter("INS_LOG_BAT_MASK", 3)
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self.set_parameter("INS_LOG_BAT_OPT", 0)
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# set the gyro filter high so we can observe behaviour
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self.set_parameter("INS_GYRO_FILTER", 100)
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self.set_parameter("LOG_BITMASK", 958)
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self.set_parameter("LOG_DISARMED", 0)
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self.set_parameter("SIM_VIB_MOT_MAX", 350)
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self.set_parameter("SIM_GYR_RND", 20)
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self.reboot_sitl()
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self.takeoff(10, mode="ALT_HOLD")
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# find a motor peak
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freq, vfr_hud, peakdb = self.hover_and_check_matched_frequency_with_fft(-15, 200, 300)
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# now add a dynamic notch and check that the peak is squashed
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self.set_parameter("INS_LOG_BAT_OPT", 2)
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self.set_parameter("INS_HNTCH_ENABLE", 1)
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self.set_parameter("INS_HNTCH_FREQ", freq)
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self.set_parameter("INS_HNTCH_REF", vfr_hud.throttle/100.)
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# first and third harmonic
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self.set_parameter("INS_HNTCH_HMNCS", 5)
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self.set_parameter("INS_HNTCH_ATT", 50)
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self.set_parameter("INS_HNTCH_BW", freq/2)
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self.reboot_sitl()
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freq, vfr_hud, peakdb1 = self.hover_and_check_matched_frequency_with_fft(-10, 20, 350, reverse=True)
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# now add double dynamic notches and check that the peak is squashed
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self.set_parameter("INS_HNTCH_OPTS", 1)
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self.reboot_sitl()
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freq, vfr_hud, peakdb2 = self.hover_and_check_matched_frequency_with_fft(-15, 20, 350, reverse=True)
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# double-notch should do better
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if peakdb2 > peakdb1:
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raise NotAchievedException("Double-notch peak was higher than single-notch peak %fdB < %fdB" % (peakdb2, peakdb1))
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except Exception as e:
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ex = e
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self.context_pop()
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if ex is not None:
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raise ex
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def hover_and_check_matched_frequency(self, dblevel=-15, minhz=200, maxhz=300, fftLength=32, peakhz=None):
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# find a motor peak
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