/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #ifndef __AP_AIRSPEED_ANALOG_H__ #define __AP_AIRSPEED_ANALOG_H__ #include #include class AP_Airspeed_Analog : public AP_Airspeed_Backend { public: AP_Airspeed_Analog(const AP_Int8 &pin) : _source(NULL), _pin(pin), _last_pin(-1) {} // probe and initialise the sensor bool init(void); // return the current differential_pressure in Pascal bool get_differential_pressure(float &pressure); // temperature not available via analog backend bool get_temperature(float &temperature) { return false; } private: AP_HAL::AnalogSource *_source; const AP_Int8 &_pin; int8_t _last_pin; }; #endif // __AP_AIRSPEED_ANALOG_H__