/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #ifndef __AP_AIRSPEED_H__ #define __AP_AIRSPEED_H__ #include #include #include #include #include class AP_Airspeed { public: // constructor AP_Airspeed(AP_AnalogSource *source) { _source = source; } // read the analog source and update _airspeed void read(void); // calibrate the airspeed. This must be called on startup if the // altitude/climb_rate/acceleration interfaces are ever used // the callback is a delay() like routine void calibrate(void (*callback)(unsigned long t)); // return the current airspeed in m/s float get_airspeed(void) { return _airspeed; } // return the current airspeed in cm/s float get_airspeed_cm(void) { return _airspeed*100; } // return true if airspeed is enabled, and airspeed use is set bool use(void) { return _enable && _use; } // return true if airspeed is enabled bool enabled(void) { return _enable; } // used by HIL to set the airspeed void set_HIL(float airspeed) { _airspeed = airspeed; } static const struct AP_Param::GroupInfo var_info[]; private: AP_AnalogSource *_source; AP_Float _offset; AP_Float _ratio; AP_Int8 _use; AP_Int8 _enable; float _airspeed; float _airspeed_raw; AverageFilterFloat_Size5 _filter; }; #endif // __AP_AIRSPEED_H__