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@ -233,81 +233,6 @@ void Copter::startup_INS_ground()
@@ -233,81 +233,6 @@ void Copter::startup_INS_ground()
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ahrs.reset(); |
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} |
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// update the harmonic notch filter center frequency dynamically
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void Copter::update_dynamic_notch(uint8_t idx) |
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{ |
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if (!ins.gyro_harmonic_notch_enabled(idx)) { |
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return; |
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} |
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const float ref_freq = ins.get_gyro_harmonic_notch_center_freq_hz(idx); |
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const float ref = ins.get_gyro_harmonic_notch_reference(idx); |
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if (is_zero(ref)) { |
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ins.update_harmonic_notch_freq_hz(idx, ref_freq); |
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return; |
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} |
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const float throttle_freq = ref_freq * MAX(1.0f, sqrtf(motors->get_throttle_out() / ref)); |
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switch (ins.get_gyro_harmonic_notch_tracking_mode(idx)) { |
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case HarmonicNotchDynamicMode::UpdateThrottle: // throttle based tracking
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// set the harmonic notch filter frequency approximately scaled on motor rpm implied by throttle
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ins.update_harmonic_notch_freq_hz(idx, throttle_freq); |
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break; |
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#if RPM_ENABLED == ENABLED |
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case HarmonicNotchDynamicMode::UpdateRPM: // rpm sensor based tracking
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case HarmonicNotchDynamicMode::UpdateRPM2: { |
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uint8_t sensor = (ins.get_gyro_harmonic_notch_tracking_mode(idx)==HarmonicNotchDynamicMode::UpdateRPM?0:1); |
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float rpm; |
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if (rpm_sensor.get_rpm(sensor, rpm)) { |
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// set the harmonic notch filter frequency from the main rotor rpm
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ins.update_harmonic_notch_freq_hz(idx, MAX(ref_freq, rpm * ref * (1.0/60))); |
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} else { |
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ins.update_harmonic_notch_freq_hz(idx, ref_freq); |
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} |
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break; |
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} |
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#endif |
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#if HAL_WITH_ESC_TELEM |
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case HarmonicNotchDynamicMode::UpdateBLHeli: // BLHeli based tracking
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// set the harmonic notch filter frequency scaled on measured frequency
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if (ins.has_harmonic_option(idx, HarmonicNotchFilterParams::Options::DynamicHarmonic)) { |
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float notches[INS_MAX_NOTCHES]; |
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const uint8_t num_notches = AP::esc_telem().get_motor_frequencies_hz(ins.get_num_gyro_dynamic_notches(idx), notches); |
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for (uint8_t i = 0; i < num_notches; i++) { |
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notches[i] = MAX(ref_freq, notches[i]); |
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} |
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if (num_notches > 0) { |
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ins.update_harmonic_notch_frequencies_hz(idx, num_notches, notches); |
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} else { // throttle fallback
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ins.update_harmonic_notch_freq_hz(idx, throttle_freq); |
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} |
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} else { |
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ins.update_harmonic_notch_freq_hz(idx, MAX(ref_freq, AP::esc_telem().get_average_motor_frequency_hz() * ref)); |
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} |
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break; |
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#endif |
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#if HAL_GYROFFT_ENABLED |
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case HarmonicNotchDynamicMode::UpdateGyroFFT: // FFT based tracking
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// set the harmonic notch filter frequency scaled on measured frequency
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if (ins.has_harmonic_option(idx, HarmonicNotchFilterParams::Options::DynamicHarmonic)) { |
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float notches[INS_MAX_NOTCHES]; |
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const uint8_t peaks = gyro_fft.get_weighted_noise_center_frequencies_hz(ins.get_num_gyro_dynamic_notches(idx), notches); |
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ins.update_harmonic_notch_frequencies_hz(idx, peaks, notches); |
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} else { |
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ins.update_harmonic_notch_freq_hz(idx, gyro_fft.get_weighted_noise_center_freq_hz()); |
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} |
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break; |
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#endif |
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case HarmonicNotchDynamicMode::Fixed: // static
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default: |
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ins.update_harmonic_notch_freq_hz(idx, ref_freq); |
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break; |
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} |
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} |
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// position_ok - returns true if the horizontal absolute position is ok and home position is set
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bool Copter::position_ok() const |
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{ |
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