// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /************************************************************ * AP_Gimbal -- library to control a 3 axis rate gimbal. * * * * Author: Arthur Benemann, Paul Riseborough; * * * ************************************************************/ #ifndef __AP_GIMBAL_H__ #define __AP_GIMBAL_H__ #include #include #if AP_AHRS_NAVEKF_AVAILABLE #include #include #include #include #include #include #include class AP_Gimbal { public: //Constructor AP_Gimbal(const AP_AHRS_NavEKF &ahrs, uint8_t compid, const AP_Mount::gimbal_params &gimbalParams) : _ekf(ahrs), _ahrs(ahrs), _gimbalParams(gimbalParams), vehicleYawRateFilt(0.0f), yawRateFiltPole(10.0f), yawErrorLimit(0.1f) { _compid = compid; } void update_target(Vector3f newTarget); void receive_feedback(mavlink_channel_t chan, mavlink_message_t *msg); void send_report(mavlink_channel_t chan) const; Vector3f getGimbalEstimateEF(); struct Measurament { float delta_time; Vector3f delta_angles; Vector3f delta_velocity; Vector3f joint_angles; } _measurement; SmallEKF _ekf; // state of small EKF for gimbal const AP_AHRS_NavEKF &_ahrs; // Main EKF Vector3f gimbalRateDemVec; // degrees/s Vector3f _angle_ef_target_rad; // desired earth-frame roll, tilt and pan angles in radians private: const AP_Mount::gimbal_params &_gimbalParams; // filtered yaw rate from the vehicle float vehicleYawRateFilt; // circular frequency (rad/sec) constant of filter applied to forward path vehicle yaw rate // this frequency must not be larger than the update rate (Hz). // reducing it makes the gimbal yaw less responsive to vehicle yaw // increasing it makes the gimbal yawe more responsive to vehicle yaw float const yawRateFiltPole; // amount of yaw angle that we permit the gimbal to lag the vehicle when operating in slave mode // reducing this makes the gimbal respond more to vehicle yaw disturbances float const yawErrorLimit; uint8_t _compid; mavlink_gimbal_report_t _report_msg; void send_control(mavlink_channel_t chan); void update_state(); void decode_feedback(mavlink_message_t *msg); bool isCopterFlipped(); // Control loop functions Vector3f getGimbalRateDemVecYaw(const Quaternion &quatEst); Vector3f getGimbalRateDemVecTilt(const Quaternion &quatEst); Vector3f getGimbalRateDemVecForward(const Quaternion &quatEst); Vector3f getGimbalRateDemVecGyroBias(); }; #endif // AP_AHRS_NAVEKF_AVAILABLE #endif // __AP_MOUNT_H__