ardupilot/libraries/AP_Soaring/Variometer.h

66 lines
1.6 KiB
C
Raw Normal View History

/* Variometer class by Samuel Tabor
Manages the estimation of aircraft total energy, drag and vertical air velocity.
*/
#pragma once
#include <AP_AHRS/AP_AHRS.h>
#include <AP_Param/AP_Param.h>
#include <AP_SpdHgtControl/AP_SpdHgtControl.h>
#include <Filter/AverageFilter.h>
#define ASPD_FILT 0.05
#define TE_FILT 0.03
#define TE_FILT_DISPLAYED 0.15
class Variometer {
const AP_Vehicle::FixedWing &_aparm;
// store time of last update
uint64_t _prev_update_time;
float _last_alt;
float _aspd_filt;
float _aspd_filt_constrained;
float _last_aspd;
float _last_roll;
float _last_total_E;
float _expected_thermalling_sink;
// declares a 5point average filter using floats
AverageFilterFloat_Size5 _vdot_filter;
AverageFilterFloat_Size5 _sp_filter;
// low pass filter @ 30s time constant
LowPassFilter<float> _climb_filter;
LowPassFilter<float> _vdot_filter2;
public:
Variometer(const AP_Vehicle::FixedWing &parms);
float alt;
float reading;
float filtered_reading;
float displayed_reading;
float raw_climb_rate;
float smoothed_climb_rate;
float tau;
void update(const float polar_K, const float polar_CD0, const float polar_B);
2019-06-23 04:52:38 -03:00
float calculate_aircraft_sinkrate(float phi, const float polar_K, const float polar_CD0, const float polar_B);
void reset_filter(float value) { _climb_filter.reset(value);}
float get_airspeed(void) {return _aspd_filt;};
float get_exp_thermalling_sink(void) {return _expected_thermalling_sink;};
float calculate_circling_time_constant();
};