mirror of https://github.com/ArduPilot/ardupilot
329 lines
12 KiB
C++
329 lines
12 KiB
C++
#pragma once
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#include "AP_Baro_config.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 <AP_Math/AP_Math.h>
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#include <Filter/DerivativeFilter.h>
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#include <AP_MSP/msp.h>
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#include <AP_ExternalAHRS/AP_ExternalAHRS.h>
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// maximum number of sensor instances
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#ifndef BARO_MAX_INSTANCES
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#define BARO_MAX_INSTANCES 3
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#endif
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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 3
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// timeouts for health reporting
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#define BARO_TIMEOUT_MS 500 // timeout in ms since last successful read
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#define BARO_DATA_CHANGE_TIMEOUT_MS 2000 // timeout in ms since last successful read that involved temperature of pressure changing
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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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friend class AP_Baro_SITL; // for access to sensors[]
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friend class AP_Baro_DroneCAN; // for access to sensors[]
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public:
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AP_Baro();
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/* Do not allow copies */
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CLASS_NO_COPY(AP_Baro);
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// get singleton
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static AP_Baro *get_singleton(void) {
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return _singleton;
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}
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// barometer types
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typedef enum {
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BARO_TYPE_AIR,
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BARO_TYPE_WATER
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} baro_type_t;
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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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#ifdef HAL_BUILD_AP_PERIPH
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// calibration and alt check not valid for AP_Periph
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bool healthy(uint8_t instance) const;
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#else
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bool healthy(uint8_t instance) const;
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#endif
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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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// returns false if we fail arming checks, in which case the buffer will be populated with a failure message
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bool arming_checks(size_t buflen, char *buffer) const;
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// get primary sensor
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uint8_t get_primary(void) const { return _primary; }
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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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#if HAL_BARO_WIND_COMP_ENABLED
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// dynamic pressure in Pascal. Divide by 100 for millibars or hectopascals
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const Vector3f& get_dynamic_pressure(uint8_t instance) const { return sensors[instance].dynamic_pressure; }
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#endif
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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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// get pressure correction in Pascal. Divide by 100 for millibars or hectopascals
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float get_pressure_correction(void) const { return get_pressure_correction(_primary); }
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float get_pressure_correction(uint8_t instance) const { return sensors[instance].p_correction; }
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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(bool save=true);
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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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// returns which i2c bus is considered "the" external bus
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uint8_t external_bus() const { return _ext_bus; }
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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 sea level pressure relative to 1976 standard atmosphere model
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// pressure in Pascal
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float get_sealevel_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;
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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[instance].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_external_temperature(void) const { return get_external_temperature(_primary); };
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float get_external_temperature(const uint8_t instance) const;
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// Set the primary baro
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void set_primary_baro(uint8_t primary) { _primary_baro.set_and_save(primary); };
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// Set the type (Air or Water) of a particular instance
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void set_type(uint8_t instance, baro_type_t type) { sensors[instance].type = type; };
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// Get the type (Air or Water) of a particular instance
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baro_type_t get_type(uint8_t instance) { return sensors[instance].type; };
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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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// set baro drift amount
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void set_baro_drift_altitude(float alt) { _alt_offset.set(alt); }
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// get baro drift amount
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float get_baro_drift_offset(void) const { return _alt_offset_active; }
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// simple atmospheric model
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static void SimpleAtmosphere(const float alt, float &sigma, float &delta, float &theta);
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// simple underwater atmospheric model
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static void SimpleUnderWaterAtmosphere(float alt, float &rho, float &delta, float &theta);
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// set a pressure correction from AP_TempCalibration
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void set_pressure_correction(uint8_t instance, float p_correction);
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uint8_t get_filter_range() const { return _filter_range; }
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// indicate which bit in LOG_BITMASK indicates baro logging enabled
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void set_log_baro_bit(uint32_t bit) { _log_baro_bit = bit; }
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bool should_log() const;
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// allow threads to lock against baro update
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HAL_Semaphore &get_semaphore(void) {
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return _rsem;
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}
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#if AP_BARO_MSP_ENABLED
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void handle_msp(const MSP::msp_baro_data_message_t &pkt);
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#endif
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#if AP_BARO_EXTERNALAHRS_ENABLED
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void handle_external(const AP_ExternalAHRS::baro_data_message_t &pkt);
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#endif
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enum Options : uint16_t {
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TreatMS5611AsMS5607 = (1U << 0U),
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};
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// check if an option is set
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bool option_enabled(const Options option) const
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{
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return (uint16_t(_options.get()) & uint16_t(option)) != 0;
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}
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private:
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// singleton
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static AP_Baro *_singleton;
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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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uint32_t _log_baro_bit = -1;
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bool init_done;
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uint8_t msp_instance_mask;
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// bitmask values for GND_PROBE_EXT
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enum {
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PROBE_BMP085=(1<<0),
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PROBE_BMP280=(1<<1),
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PROBE_MS5611=(1<<2),
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PROBE_MS5607=(1<<3),
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PROBE_MS5637=(1<<4),
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PROBE_FBM320=(1<<5),
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PROBE_DPS280=(1<<6),
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PROBE_LPS25H=(1<<7),
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PROBE_KELLER=(1<<8),
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PROBE_MS5837=(1<<9),
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PROBE_BMP388=(1<<10),
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PROBE_SPL06 =(1<<11),
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PROBE_MSP =(1<<12),
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};
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#if HAL_BARO_WIND_COMP_ENABLED
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class WindCoeff {
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public:
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static const struct AP_Param::GroupInfo var_info[];
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AP_Int8 enable; // enable compensation for this barometer
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AP_Float xp; // ratio of static pressure rise to dynamic pressure when flying forwards
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AP_Float xn; // ratio of static pressure rise to dynamic pressure when flying backwards
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AP_Float yp; // ratio of static pressure rise to dynamic pressure when flying to the right
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AP_Float yn; // ratio of static pressure rise to dynamic pressure when flying to the left
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AP_Float zp; // ratio of static pressure rise to dynamic pressure when flying up
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AP_Float zn; // ratio of static pressure rise to dynamic pressure when flying down
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};
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#endif
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struct sensor {
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uint32_t last_update_ms; // last update time in ms
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uint32_t last_change_ms; // last update time in ms that included a change in reading from previous readings
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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_pressure;
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float p_correction;
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baro_type_t type; // 0 for air pressure (default), 1 for water pressure
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bool healthy; // true if sensor is healthy
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bool alt_ok; // true if calculated altitude is ok
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bool calibrated; // true if calculated calibrated successfully
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AP_Int32 bus_id;
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#if HAL_BARO_WIND_COMP_ENABLED
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WindCoeff wind_coeff;
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Vector3f dynamic_pressure; // calculated dynamic pressure
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#endif
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} sensors[BARO_MAX_INSTANCES];
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AP_Float _alt_offset;
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float _alt_offset_active;
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AP_Float _field_elevation; // field elevation in meters
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float _field_elevation_active;
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uint32_t _field_elevation_last_ms;
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AP_Int8 _primary_baro; // primary chosen by user
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AP_Int8 _ext_bus; // bus number for external barometer
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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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AP_Float _specific_gravity; // the specific gravity of fluid for an ROV 1.00 for freshwater, 1.024 for salt water
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AP_Float _user_ground_temperature; // user override of the ground temperature used for EAS2TAS
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float _guessed_ground_temperature; // currently ground temperature estimate using our best available source
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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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// see if we already have probed a i2c driver by bus number and address
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bool _have_i2c_driver(uint8_t bus_num, uint8_t address) const;
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bool _add_backend(AP_Baro_Backend *backend);
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void _probe_i2c_barometers(void);
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AP_Int8 _filter_range; // valid value range from mean value
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AP_Int32 _baro_probe_ext;
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#ifndef HAL_BUILD_AP_PERIPH
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AP_Float _alt_error_max;
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#endif
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AP_Int16 _options;
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// semaphore for API access from threads
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HAL_Semaphore _rsem;
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#if HAL_BARO_WIND_COMP_ENABLED
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/*
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return pressure correction for wind based on GND_WCOEF parameters
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*/
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float wind_pressure_correction(uint8_t instance);
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#endif
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// Logging function
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void Write_Baro(void);
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void Write_Baro_instance(uint64_t time_us, uint8_t baro_instance);
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void update_field_elevation();
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};
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namespace AP {
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AP_Baro &baro();
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};
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