mirror of https://github.com/ArduPilot/ardupilot
AP_Gimbal: clean-up for AP_Mount merge
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@ -2,24 +2,15 @@
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#include <stdio.h>
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#include <AP_Common.h>
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#include <AP_Progmem.h>
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#include <AP_Param.h>
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#include <AP_Gimbal.h>
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#include <GCS.h>
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#include <GCS_MAVLink.h>
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#include <AP_SmallEKF.h>
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const AP_Param::GroupInfo AP_Gimbal::var_info[] PROGMEM = {
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AP_GROUPEND
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};
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uint16_t feedback_error_count;
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static float K_gimbalRate = 5.0f;
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static float angRateLimit = 0.5f;
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void AP_Gimbal::receive_feedback(mavlink_channel_t chan, mavlink_message_t *msg)
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{
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update_targets_from_rc();
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decode_feedback(msg);
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update_state();
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if (_ekf.getStatus() && !isCopterFliped()){
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@ -168,32 +159,11 @@ void AP_Gimbal::send_control(mavlink_channel_t chan)
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}
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void AP_Gimbal::update_failsafe(uint8_t rc_failsafe)
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void AP_Gimbal::update_failsafe(uint8_t failsafe)
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{
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_rc_failsafe = rc_failsafe;
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_failsafe = failsafe;
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}
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// returns the angle (radians) that the RC_Channel input is receiving
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float angle_input_rad(RC_Channel* rc, float angle_min, float angle_max)
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{
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float input =rc->norm_input();
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float angle = input*(angle_max - angle_min) + angle_min;
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return radians(angle);
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}
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// update_targets_from_rc - updates angle targets using input from receiver
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void AP_Gimbal::update_targets_from_rc()
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{
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// Get new tilt angle
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float new_tilt = (_rc_failsafe)?0.0f:angle_input_rad(RC_Channel::rc_channel(tilt_rc_in-1), _tilt_angle_min, _tilt_angle_max);
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// Low-pass filter
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new_tilt = _angle_ef_target_rad.y + 0.09f*(new_tilt - _angle_ef_target_rad.y);
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// Slew-rate constrain
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float max_change_rads =_max_tilt_rate * _measurament.delta_time;
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float tilt_change = constrain_float(new_tilt - _angle_ef_target_rad.y,-max_change_rads,+max_change_rads);
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// Update tilt
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_angle_ef_target_rad.y = constrain_float(_angle_ef_target_rad.y + tilt_change,_tilt_angle_min,_tilt_angle_max);
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}
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uint8_t AP_Gimbal::isCopterFliped(){
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return fabs(_ahrs.roll)>1.0f || fabs(_ahrs.pitch)>1.0f;
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@ -28,29 +28,21 @@ class AP_Gimbal
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public:
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//Constructor
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AP_Gimbal(const AP_AHRS_NavEKF &ahrs, uint8_t sysid, uint8_t compid) :
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_ahrs(ahrs),
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_ekf(ahrs),
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_ahrs(ahrs),
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_joint_offsets(0.0f,0.0f,0.0f),
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vehicleYawRateFilt(0.0f),
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yawRateFiltPole(10.0f),
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yawErrorLimit(0.1f),
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tilt_rc_in(6),
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_tilt_angle_min(-45.0f),
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_tilt_angle_max(0.0f),
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_max_tilt_rate(0.5f),
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_rc_failsafe(true)
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_failsafe(true)
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{
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AP_Param::setup_object_defaults(this, var_info);
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_sysid = sysid;
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_compid = compid;
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}
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void update_failsafe(uint8_t rc_failsafe);
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void update_failsafe(uint8_t failsafe);
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void receive_feedback(mavlink_channel_t chan, mavlink_message_t *msg);
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// hook for eeprom variables
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static const struct AP_Param::GroupInfo var_info[];
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struct Measurament {
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float delta_time;
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Vector3f delta_angles;
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@ -59,10 +51,15 @@ public:
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} _measurament;
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SmallEKF _ekf; // state of small EKF for gimbal
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const AP_AHRS_NavEKF &_ahrs; // Main EKF
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Vector3f gimbalRateDemVec; // degrees/s
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Vector3f _angle_ef_target_rad; // desired earth-frame roll, tilt and pan angles in radians
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private:
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// These are corrections (in radians) applied to the to the gimbal joint (x,y,z = roll,pitch,yaw) measurements
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Vector3f const _joint_offsets;
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// filtered yaw rate from the vehicle
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float vehicleYawRateFilt;
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@ -76,26 +73,15 @@ private:
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// reducing this makes the gimbal respond more to vehicle yaw disturbances
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float const yawErrorLimit;
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// These are corrections (in radians) applied to the to the gimbal joint (x,y,z = roll,pitch,yaw) measurements
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Vector3f const _joint_offsets;
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// status of the RC signal
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uint8_t _failsafe;
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uint8_t const tilt_rc_in;
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float const _tilt_angle_min; // min tilt in 0.01 degree units
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float const _tilt_angle_max; // max tilt in 0.01 degree units
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float const _max_tilt_rate; // max tilt rate in rad/s
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const AP_AHRS_NavEKF &_ahrs; // Main EKF
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uint8_t _sysid;
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uint8_t _compid;
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uint8_t _rc_failsafe; // status of the RC signal
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void send_control(mavlink_channel_t chan);
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void update_state();
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void decode_feedback(mavlink_message_t *msg);
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void update_targets_from_rc();
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uint8_t isCopterFliped();
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