// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*- /// @file AP_SpdHgtControl.h /// @brief generic speed & height controller interface /* This defines a generic interface for speed & height controllers. Each specific controller should be a subclass of this generic interface. All variables used by controllers should be in their own class. */ #ifndef AP_SPDHGTCONTROL_H #define AP_SPDHGTCONTROL_H #include #include #include class AP_SpdHgtControl { public: // Update the internal state of the height and height rate estimator // Update of the inertial speed rate estimate internal state // Should be called at 50Hz or faster virtual void update_50hz(float height_above_field) = 0; /** stages of flight so the altitude controller can choose to prioritise height or speed */ enum FlightStage { FLIGHT_NORMAL = 1, FLIGHT_TAKEOFF = 2, FLIGHT_LAND_APPROACH = 3, FLIGHT_LAND_FINAL = 4 }; // Update of the pitch and throttle demands // Should be called at 10Hz or faster virtual void update_pitch_throttle( int32_t hgt_dem_cm, int32_t EAS_dem_cm, enum FlightStage flight_stage, int32_t ptchMinCO_cd, int16_t throttle_nudge, float hgt_afe) = 0; // demanded throttle in percentage // should return 0 to 100 virtual int32_t get_throttle_demand(void)=0; // demanded pitch angle in centi-degrees // should return -9000 to +9000 virtual int32_t get_pitch_demand(void)=0; // Rate of change of velocity along X body axis in m/s^2 virtual float get_VXdot(void)=0; // log data on internal state of the controller. Called at 10Hz virtual void log_data(DataFlash_Class &dataflash, uint8_t msgid) = 0; // return current target airspeed virtual float get_target_airspeed(void) const = 0; // return maximum climb rate virtual float get_max_climbrate(void) const = 0; // add new controllers to this enum. Users can then // select which controller to use by setting the // SPDHGT_CONTROLLER parameter enum ControllerType { CONTROLLER_TECS = 1 }; }; #endif // AP_SPDHGTCONTROL_H