mirror of https://github.com/ArduPilot/ardupilot
174 lines
6.4 KiB
C++
174 lines
6.4 KiB
C++
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#ifndef __AP_BARO_H__
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#define __AP_BARO_H__
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#include <AP_HAL/AP_HAL.h>
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#include <AP_Param/AP_Param.h>
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#include <Filter/Filter.h>
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#include <Filter/DerivativeFilter.h>
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#include <AP_Buffer/AP_Buffer.h>
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// maximum number of sensor instances
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#define BARO_MAX_INSTANCES 3
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// maximum number of drivers. Note that a single driver can provide
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// multiple sensor instances
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#define BARO_MAX_DRIVERS 2
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class AP_Baro_Backend;
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class AP_Baro
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{
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friend class AP_Baro_Backend;
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public:
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// constructor
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AP_Baro();
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// initialise the barometer object, loading backend drivers
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void init(void);
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// update the barometer object, asking backends to push data to
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// the frontend
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void update(void);
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// healthy - returns true if sensor and derived altitude are good
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bool healthy(void) const { return healthy(_primary); }
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bool healthy(uint8_t instance) const { return sensors[instance].healthy && sensors[instance].alt_ok && sensors[instance].calibrated; }
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// check if all baros are healthy - used for SYS_STATUS report
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bool all_healthy(void) const;
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// pressure in Pascal. Divide by 100 for millibars or hectopascals
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float get_pressure(void) const { return get_pressure(_primary); }
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float get_pressure(uint8_t instance) const { return sensors[instance].pressure; }
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// temperature in degrees C
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float get_temperature(void) const { return get_temperature(_primary); }
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float get_temperature(uint8_t instance) const { return sensors[instance].temperature; }
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// accumulate a reading on sensors. Some backends without their
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// own thread or a timer may need this.
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void accumulate(void);
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// calibrate the barometer. This must be called on startup if the
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// altitude/climb_rate/acceleration interfaces are ever used
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void calibrate(void);
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// update the barometer calibration to the current pressure. Can
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// be used for incremental preflight update of baro
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void update_calibration(void);
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// get current altitude in meters relative to altitude at the time
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// of the last calibrate() call
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float get_altitude(void) const { return get_altitude(_primary); }
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float get_altitude(uint8_t instance) const { return sensors[instance].altitude; }
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// get altitude difference in meters relative given a base
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// pressure in Pascal
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float get_altitude_difference(float base_pressure, float pressure) const;
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// get scale factor required to convert equivalent to true airspeed
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float get_EAS2TAS(void);
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// get air density / sea level density - decreases as altitude climbs
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float get_air_density_ratio(void);
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// get current climb rate in meters/s. A positive number means
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// going up
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float get_climb_rate(void);
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// ground temperature in degrees C
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// the ground values are only valid after calibration
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float get_ground_temperature(void) const { return get_ground_temperature(_primary); }
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float get_ground_temperature(uint8_t i) const { return sensors[i].ground_temperature.get(); }
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// ground pressure in Pascal
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// the ground values are only valid after calibration
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float get_ground_pressure(void) const { return get_ground_pressure(_primary); }
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float get_ground_pressure(uint8_t i) const { return sensors[i].ground_pressure.get(); }
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// set the temperature to be used for altitude calibration. This
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// allows an external temperature source (such as a digital
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// airspeed sensor) to be used as the temperature source
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void set_external_temperature(float temperature);
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// get last time sample was taken (in ms)
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uint32_t get_last_update(void) const { return get_last_update(_primary); }
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uint32_t get_last_update(uint8_t instance) const { return sensors[_primary].last_update_ms; }
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// settable parameters
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static const struct AP_Param::GroupInfo var_info[];
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float get_calibration_temperature(void) const { return get_calibration_temperature(_primary); }
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float get_calibration_temperature(uint8_t instance) const;
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// HIL (and SITL) interface, setting altitude
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void setHIL(float altitude_msl);
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// HIL (and SITL) interface, setting pressure and temperature
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void setHIL(uint8_t instance, float pressure, float temperature);
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// HIL variables
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struct {
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AP_Buffer<float,10> press_buffer;
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AP_Buffer<float,10> temp_buffer;
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} _hil;
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// register a new sensor, claiming a sensor slot. If we are out of
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// slots it will panic
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uint8_t register_sensor(void);
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// return number of registered sensors
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uint8_t num_instances(void) const { return _num_sensors; }
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// enable HIL mode
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void set_hil_mode(void) { _hil_mode = true; }
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private:
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// how many drivers do we have?
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uint8_t _num_drivers;
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AP_Baro_Backend *drivers[BARO_MAX_DRIVERS];
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// how many sensors do we have?
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uint8_t _num_sensors;
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// what is the primary sensor at the moment?
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uint8_t _primary;
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struct sensor {
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uint32_t last_update_ms; // last update time in ms
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bool healthy:1; // true if sensor is healthy
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bool alt_ok:1; // true if calculated altitude is ok
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bool calibrated:1; // true if calculated calibrated successfully
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float pressure; // pressure in Pascal
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float temperature; // temperature in degrees C
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float altitude; // calculated altitude
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AP_Float ground_temperature;
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AP_Float ground_pressure;
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} sensors[BARO_MAX_INSTANCES];
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AP_Float _alt_offset;
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AP_Int8 _primary_baro; // primary chosen by user
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float _last_altitude_EAS2TAS;
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float _EAS2TAS;
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float _external_temperature;
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uint32_t _last_external_temperature_ms;
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DerivativeFilterFloat_Size7 _climb_rate_filter;
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bool _hil_mode:1;
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// when did we last notify the GCS of new pressure reference?
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uint32_t _last_notify_ms;
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void SimpleAtmosphere(const float alt, float &sigma, float &delta, float &theta);
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};
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#include "AP_Baro_Backend.h"
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#include "AP_Baro_MS5611.h"
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#include "AP_Baro_BMP085.h"
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#include "AP_Baro_HIL.h"
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#include "AP_Baro_PX4.h"
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#endif // __AP_BARO_H__
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