ardupilot/libraries/AP_Mount/AP_Gimbal.h

95 lines
2.9 KiB
C++

// -*- 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 <AP_HAL.h>
#include <AP_AHRS.h>
#if AP_AHRS_NAVEKF_AVAILABLE
#include <AP_Math.h>
#include <AP_Common.h>
#include <AP_GPS.h>
#include <GCS_MAVLink.h>
#include <AP_Mount.h>
#include <AP_SmallEKF.h>
#include <AP_NavEKF.h>
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__