mirror of https://github.com/ArduPilot/ardupilot
72 lines
2.0 KiB
C++
72 lines
2.0 KiB
C++
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/* Variometer class by Samuel Tabor
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Manages the estimation of aircraft total energy, drag and vertical air velocity.
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*/
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#pragma once
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#include <AP_AHRS/AP_AHRS.h>
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#include <AP_Param/AP_Param.h>
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#include <Filter/AverageFilter.h>
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#include <AP_Vehicle/AP_Vehicle.h>
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class Variometer {
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const AP_Vehicle::FixedWing &_aparm;
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// store time of last update
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uint64_t _prev_update_time;
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float _raw_climb_rate;
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float _aspd_filt_constrained;
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float _expected_thermalling_sink;
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// declares a 5point average filter using floats
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AverageFilterFloat_Size5 _vdot_filter;
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AverageFilterFloat_Size5 _sp_filter;
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/*
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low pass filters for various purposes.
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*/
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// Climb rate filter for monitoring progress in thermal.
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LowPassFilter<float> _climb_filter{1/60.0};
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// Fast filter for mavlink/audio vario output.
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LowPassFilter<float> _audio_filter{1/0.71};
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// Slower filter for deciding to enter THERMAL mode.
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LowPassFilter<float> _trigger_filter{1/4.06};
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// Longitudinal acceleration bias filter.
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LowPassFilter<float> _vdotbias_filter{1/60.0};
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public:
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Variometer(const AP_Vehicle::FixedWing &parms);
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float alt;
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float reading;
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float tau;
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void update(const float thermal_bank, const float polar_K, const float polar_CD0, const float polar_B);
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float calculate_aircraft_sinkrate(float phi, const float polar_K, const float polar_CD0, const float polar_B) const;
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void reset_climb_filter(float value) { _climb_filter.reset(value);}
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void reset_trigger_filter(float value) { _trigger_filter.reset(value);}
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float get_airspeed(void) const {return _aspd_filt_constrained;};
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float get_displayed_value(void) const {return _audio_filter.get();};
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float get_filtered_climb(void) const {return _climb_filter.get();};
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float get_trigger_value(void) const {return _trigger_filter.get();};
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float get_exp_thermalling_sink(void) const {return _expected_thermalling_sink;};
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float calculate_circling_time_constant(const float thermal_bank);
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};
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