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163 lines
6.2 KiB
163 lines
6.2 KiB
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- |
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#pragma once |
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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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