// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /* MAVLink enabled mount backend class */ #ifndef __AP_MOUNT_MAVLINK_H__ #define __AP_MOUNT_MAVLINK_H__ #include #include #if AP_AHRS_NAVEKF_AVAILABLE #include #include #include #include #include #include #include class AP_Mount_MAVLink : public AP_Mount_Backend { public: // Constructor AP_Mount_MAVLink(AP_Mount &frontend, AP_Mount::mount_state &state, uint8_t instance); // init - performs any required initialisation for this instance virtual void init(const AP_SerialManager& serial_manager); // update mount position - should be called periodically virtual void update(); // has_pan_control - returns true if this mount can control it's pan (required for multicopters) virtual bool has_pan_control() const; // set_mode - sets mount's mode virtual void set_mode(enum MAV_MOUNT_MODE mode); // status_msg - called to allow mounts to send their status to GCS using the MOUNT_STATUS message virtual void status_msg(mavlink_channel_t chan); // handle a GIMBAL_REPORT message virtual void handle_gimbal_report(mavlink_channel_t chan, mavlink_message_t *msg); // send a GIMBAL_REPORT message to the GCS virtual void send_gimbal_report(mavlink_channel_t chan); private: // internal variables bool _initialised; // true once the driver has been initialised // state of small EKF for gimbal SmallEKF _ekf; // keep last gimbal report mavlink_gimbal_report_t _gimbal_report; float vehicleYawRateFilt; const float K_gimbalRate; const float angRateLimit; // 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 const float 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 const float yawErrorLimit; // quaternion demanded at the previous time step Quaternion lastQuatDem; Vector3f quaternion_to_vector(const Quaternion &quat); Matrix3f vector312_to_rotation_matrix(const Vector3f &vector); Vector3f gimbal_update_control1(const Vector3f &ef_target_euler_rad, float delta_time, const Vector3f &delta_angles, const Vector3f &delta_velocity, const Vector3f &joint_angles); Vector3f gimbal_update_control2(const Vector3f &ef_target_euler_rad, float delta_time, const Vector3f &delta_angles, const Vector3f &delta_velocity, const Vector3f &joint_angles); Vector3f getGimbalRateDemVecYaw(const Vector3f &ef_target_euler_rad, float delta_time, const Quaternion &quatEst, const Vector3f &joint_angles); Vector3f getGimbalRateDemVecTilt(const Vector3f &ef_target_euler_rad, const Quaternion &quatEst); Vector3f getGimbalRateDemVecForward(const Vector3f &ef_target_euler_rad, float delta_time, const Quaternion &quatEst); }; #endif // AP_AHRS_NAVEKF_AVAILABLE #endif // __AP_MOUNT_MAVLINK_H__