ardupilot/libraries/SITL/SIM_Gimbal.h

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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
*/
/*
gimbal simulator class
*/
#ifndef _SIM_GIMBAL_H
#define _SIM_GIMBAL_H
#include "SIM_Aircraft.h"
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
#include <AP_HAL/utility/Socket.h>
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class Gimbal
{
public:
Gimbal(const struct sitl_fdm &_fdm);
void update(void);
private:
const struct sitl_fdm &fdm;
const char *target_address;
const uint16_t target_port;
// rotation matrix (gimbal body -> earth)
Matrix3f dcm;
// time of last update
uint32_t last_update_us;
// true angular rate of gimbal in body frame (rad/s)
Vector3f gimbal_angular_rate;
// observed angular rate (including biases)
Vector3f gyro;
/* joint angles, in radians. in yaw/roll/pitch order. Relative to fwd.
So 0,0,0 points forward.
Pi/2,0,0 means pointing right
0, Pi/2, 0 means pointing fwd, but rolled 90 degrees to right
0, 0, -Pi/2, means pointing down
*/
Vector3f joint_angles;
// physical constraints on joint angles in (roll, pitch, azimuth) order
Vector3f lower_joint_limits;
Vector3f upper_joint_limits;
const float travelLimitGain;
// true gyro bias
Vector3f true_gyro_bias;
// reporting variables. gimbal pushes these to vehicle code over
// MAVLink at approx 100Hz
// reporting period in ms
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const float reporting_period_ms;
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// integral of gyro vector over last time interval. In radians
Vector3f delta_angle;
// integral of accel vector over last time interval. In m/s
Vector3f delta_velocity;
/*
control variables from the vehicle
*/
// angular rate in rad/s. In body frame of gimbal
Vector3f demanded_angular_rate;
// gyro bias provided by EKF on vehicle. In rad/s.
// Should be subtracted from the gyro readings to get true body
// rotatation rates
Vector3f supplied_gyro_bias;
uint32_t last_report_us;
uint32_t last_heartbeat_ms;
bool seen_heartbeat;
bool seen_gimbal_control;
uint8_t vehicle_system_id;
uint8_t vehicle_component_id;
SocketAPM mav_socket;
struct {
// socket to telem2 on aircraft
bool connected;
mavlink_message_t rxmsg;
mavlink_status_t status;
uint8_t seq;
} mavlink;
void send_report(void);
};
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#endif // CONFIG_HAL_BOARD
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#endif // _SIM_GIMBAL_H