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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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Merge remote-tracking branch 'upstream/master' into swissfang
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@@ -910,12 +910,14 @@ MPU6000::ioctl(struct file *filp, int cmd, unsigned long arg)
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// adjust filters
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float cutoff_freq_hz = _accel_filter_x.get_cutoff_freq();
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float sample_rate = 1.0e6f/ticks;
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_set_dlpf_filter(cutoff_freq_hz);
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_accel_filter_x.set_cutoff_frequency(sample_rate, cutoff_freq_hz);
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_accel_filter_y.set_cutoff_frequency(sample_rate, cutoff_freq_hz);
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_accel_filter_z.set_cutoff_frequency(sample_rate, cutoff_freq_hz);
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float cutoff_freq_hz_gyro = _gyro_filter_x.get_cutoff_freq();
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_set_dlpf_filter(cutoff_freq_hz_gyro);
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_gyro_filter_x.set_cutoff_frequency(sample_rate, cutoff_freq_hz_gyro);
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_gyro_filter_y.set_cutoff_frequency(sample_rate, cutoff_freq_hz_gyro);
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_gyro_filter_z.set_cutoff_frequency(sample_rate, cutoff_freq_hz_gyro);
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@@ -968,11 +970,9 @@ MPU6000::ioctl(struct file *filp, int cmd, unsigned long arg)
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return _accel_filter_x.get_cutoff_freq();
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case ACCELIOCSLOWPASS:
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if (arg == 0) {
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// allow disabling of on-chip filter using
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// zero as desired filter frequency
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_set_dlpf_filter(0);
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}
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// set hardware filtering
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_set_dlpf_filter(arg);
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// set software filtering
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_accel_filter_x.set_cutoff_frequency(1.0e6f / _call_interval, arg);
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_accel_filter_y.set_cutoff_frequency(1.0e6f / _call_interval, arg);
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_accel_filter_z.set_cutoff_frequency(1.0e6f / _call_interval, arg);
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@@ -1053,14 +1053,11 @@ MPU6000::gyro_ioctl(struct file *filp, int cmd, unsigned long arg)
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case GYROIOCGLOWPASS:
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return _gyro_filter_x.get_cutoff_freq();
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case GYROIOCSLOWPASS:
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// set hardware filtering
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_set_dlpf_filter(arg);
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_gyro_filter_x.set_cutoff_frequency(1.0e6f / _call_interval, arg);
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_gyro_filter_y.set_cutoff_frequency(1.0e6f / _call_interval, arg);
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_gyro_filter_z.set_cutoff_frequency(1.0e6f / _call_interval, arg);
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if (arg == 0) {
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// allow disabling of on-chip filter using 0
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// as desired frequency
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_set_dlpf_filter(0);
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}
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return OK;
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case GYROIOCSSCALE:
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@@ -295,6 +295,7 @@ private:
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float _battery_amp_bias; ///< current sensor bias
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float _battery_mamphour_total;///< amp hours consumed so far
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uint64_t _battery_last_timestamp;///< last amp hour calculation timestamp
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bool _cb_flighttermination; ///< true if the flight termination circuit breaker is enabled
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#ifdef CONFIG_ARCH_BOARD_PX4FMU_V1
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bool _dsm_vcc_ctl; ///< true if relay 1 controls DSM satellite RX power
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@@ -515,7 +516,8 @@ PX4IO::PX4IO(device::Device *interface) :
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_battery_amp_per_volt(90.0f / 5.0f), // this matches the 3DR current sensor
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_battery_amp_bias(0),
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_battery_mamphour_total(0),
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_battery_last_timestamp(0)
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_battery_last_timestamp(0),
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_cb_flighttermination(true)
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#ifdef CONFIG_ARCH_BOARD_PX4FMU_V1
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, _dsm_vcc_ctl(false)
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#endif
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@@ -1051,6 +1053,9 @@ PX4IO::task_main()
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}
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}
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/* Update Circuit breakers */
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_cb_flighttermination = circuit_breaker_enabled("CBRK_FLIGHTTERM", CBRK_FLIGHTTERM_KEY);
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}
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}
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@@ -1170,7 +1175,7 @@ PX4IO::io_set_arming_state()
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}
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/* Do not set failsafe if circuit breaker is enabled */
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if (armed.force_failsafe && !circuit_breaker_enabled("CBRK_FLIGHTTERM", CBRK_FLIGHTTERM_KEY)) {
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if (armed.force_failsafe && !_cb_flighttermination) {
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set |= PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE;
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} else {
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clear |= PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE;
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