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This is the initial implementation of Alemox gimbal protocol. the uart output is for the moment hard coded but should become a parameter.master
Matthias Badaire
10 years ago
committed by
Andrew Tridgell
2 changed files with 558 additions and 0 deletions
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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#include "AP_Mount_Alexmos.h" |
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extern const AP_HAL::HAL& hal; |
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void AP_Mount_Alexmos::init (){ |
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_board_version = 0; |
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_current_firmware_version = 0.0f; |
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_firmware_beta_version = 0; |
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_port = hal.uartE;
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_port->begin(115200); |
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_initialised = true;
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_step = 0; |
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_param_read_once=false; |
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get_boardinfo(); |
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read_params(0); //we request parameters for profile 0 and therfore get global and profile parameters
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} |
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// update mount position - should be called periodically
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void AP_Mount_Alexmos::update() |
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{ |
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if (!_initialised){ |
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return; |
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} |
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read_incoming(); // read the incoming messages from the gimbal
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// update based on mount mode
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switch(_frontend.get_mode(_instance)) { |
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// move mount to a "retracted" position. we do not implement a separate servo based retract mechanism
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case MAV_MOUNT_MODE_RETRACT: |
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control_axis(_frontend.state[_instance]._retract_angles.get(), true); |
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break; |
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// move mount to a neutral position, typically pointing forward
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case MAV_MOUNT_MODE_NEUTRAL: |
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control_axis(_frontend.state[_instance]._neutral_angles.get(), true); |
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break; |
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// point to the angles given by a mavlink message
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case MAV_MOUNT_MODE_MAVLINK_TARGETING: |
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// do nothing because earth-frame angle targets (i.e. _angle_ef_target_rad) should have already been set by a MOUNT_CONTROL message from GCS
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break; |
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// RC radio manual angle control, but with stabilization from the AHRS
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case MAV_MOUNT_MODE_RC_TARGETING: |
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// update targets using pilot's rc inputs
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update_targets_from_rc(); |
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control_axis(_angle_ef_target_rad, false); |
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break; |
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// point mount to a GPS point given by the mission planner
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case MAV_MOUNT_MODE_GPS_POINT: |
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if(_frontend._ahrs.get_gps().status() >= AP_GPS::GPS_OK_FIX_2D) { |
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calc_angle_to_location(_frontend.state[_instance]._roi_target, _angle_ef_target_rad, true, false); |
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control_axis(_angle_ef_target_rad, false); |
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} |
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break; |
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default: |
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// we do not know this mode so do nothing
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break; |
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} |
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} |
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// has_pan_control - returns true if this mount can control it's pan (required for multicopters)
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bool AP_Mount_Alexmos::has_pan_control() const |
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{ |
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return _gimbal_3axis; |
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} |
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// set_mode - sets mount's mode
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void AP_Mount_Alexmos::set_mode(enum MAV_MOUNT_MODE mode) |
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{ |
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// record the mode change and return success
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_frontend.state[_instance]._mode = mode; |
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} |
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// status_msg - called to allow mounts to send their status to GCS using the MOUNT_STATUS message
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void AP_Mount_Alexmos::status_msg(mavlink_channel_t chan) |
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{ |
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mavlink_msg_mount_status_send(chan, 0, 0, _current_angle.x*100, _current_angle.y*100, _current_angle.z*100); |
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} |
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/*
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* get_angles () |
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*/ |
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void AP_Mount_Alexmos::get_angles( ){ |
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uint8_t data[1] = {(uint8_t)1}; |
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send_command (CMD_GET_ANGLES, data , 1); |
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} |
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/*
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* set_motor will activate motors if true , and disable them if false. |
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*/ |
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void AP_Mount_Alexmos::set_motor(bool on){ |
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if ( on ){ |
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uint8_t data[1] = {(uint8_t)1}; |
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send_command (CMD_MOTORS_ON, data , 1); |
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} else { |
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uint8_t data[1] = {(uint8_t)1}; |
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send_command (CMD_MOTORS_OFF, data , 1); |
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} |
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} |
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/*
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* get board version and firmware version |
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*/ |
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void AP_Mount_Alexmos::get_boardinfo(){ |
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if (_board_version != 0) |
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return ; |
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uint8_t data[1] = {(uint8_t)1}; |
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send_command (CMD_BOARD_INFO, data , 1); |
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} |
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void AP_Mount_Alexmos::control_axis(const Vector3f& angle, bool target_in_degrees ){ |
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// convert to degrees if necessary
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Vector3f target_deg = angle; |
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if (!target_in_degrees) { |
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target_deg *= RAD_TO_DEG; |
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} |
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uint8_t mode = MODE_ANGLE; |
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int16_t speed_roll = DEGREE_PER_SEC_TO_VALUE(SPEED); |
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int16_t angle_roll = DEGREE_TO_VALUE(target_deg.x); |
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int16_t speed_pitch = DEGREE_PER_SEC_TO_VALUE(SPEED); |
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int16_t angle_pitch = DEGREE_TO_VALUE(target_deg.y); |
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int16_t speed_yaw = DEGREE_PER_SEC_TO_VALUE(SPEED); |
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int16_t angle_yaw = DEGREE_TO_VALUE(target_deg.z); |
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uint8_t data[13] = { |
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(uint8_t)mode,
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(uint8_t)speed_roll , (uint8_t)(speed_roll >> 8) , |
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(uint8_t)angle_roll , (uint8_t)(angle_roll >> 8 ), |
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(uint8_t)speed_pitch , (uint8_t)(speed_pitch >> 8) , |
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(uint8_t)angle_pitch , (uint8_t)(angle_pitch >> 8) , |
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(uint8_t)speed_yaw , (uint8_t)(speed_yaw >> 8 ), |
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(uint8_t)angle_yaw , (uint8_t)(angle_yaw >> 8)
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}; |
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send_command (CMD_CONTROL, data , 13); |
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} |
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/*
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read current profile profile_id and global parameters from the gimbal settings |
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*/ |
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void AP_Mount_Alexmos::read_params (uint8_t profile_id){ |
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uint8_t data[1] = {(uint8_t) profile_id};
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send_command (CMD_READ_PARAMS, data , 1); |
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} |
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/*
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write new parameters to the gimbal settings |
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*/ |
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void AP_Mount_Alexmos::write_params (){ |
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if (!_param_read_once)
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return; |
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send_command (CMD_WRITE_PARAMS, _current_parameters.bytes , sizeof (alexmos_params)); |
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} |
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/*
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send a command to the Alemox Serial API
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*/ |
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void AP_Mount_Alexmos::send_command(uint8_t cmd, uint8_t* data, uint8_t size){ |
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if (_port->txspace() < (size + 5)){ |
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return; |
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} |
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uint8_t checksum = 0; |
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_port->write( '>' ); |
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_port->write( cmd ); // write command id
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_port->write( size ); // write body size
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_port->write( cmd+size ); // write header checkum
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for (uint8_t i = 0; i != size ; i++){ |
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checksum += data[i]; |
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_port->write ( data[i] ); |
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} |
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_port->write (checksum); |
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} |
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/*
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* Parse the body of the message received from the Alexmos gimbal |
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*/
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void AP_Mount_Alexmos::parse_body (){ |
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switch (_command_id ){ |
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case CMD_BOARD_INFO: |
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_board_version = _buffer.version._board_version/ 10; |
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_current_firmware_version = _buffer.version._firmware_version / 1000.0f ; |
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_firmware_beta_version = _buffer.version._firmware_version % 10 ; |
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_gimbal_3axis = ( _buffer.version._board_features & 0x1 ); |
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_gimbal_bat_monitoring = (_buffer.version._board_features & 0x2 ); |
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break; |
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case CMD_GET_ANGLES: |
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_current_angle.x = VALUE_TO_DEGREE(_buffer.angles.angle_roll); |
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_current_angle.y = VALUE_TO_DEGREE(_buffer.angles.angle_pitch); |
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_current_angle.z = VALUE_TO_DEGREE(_buffer.angles.angle_yaw); |
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break; |
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case CMD_READ_PARAMS: |
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_param_read_once = true; |
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_current_parameters.params = _buffer.params; |
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break; |
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case CMD_WRITE_PARAMS: |
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break; |
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default : |
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_last_command_confirmed = true; |
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break; |
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} |
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} |
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/*
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* detect and read the header of the incoming message from the gimbal |
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*/ |
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void AP_Mount_Alexmos::read_incoming (){ |
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uint8_t data ; |
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while (_port->available()){ |
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data = _port->read(); |
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switch (_step){ |
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case 0: |
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if ( '>' == data){ |
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_step = 1; |
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_checksum = 0; //reset checksum accumulator
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_last_command_confirmed = false; |
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} |
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break; |
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case 1:// command ID
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_checksum = data; |
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_command_id = data; |
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_step++; |
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break; |
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case 2: // Size of the body of the message
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_checksum += data; |
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_payload_length = data; |
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_step++; |
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break;
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case 3: // checksum of the header
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if (_checksum != data ) { |
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_step = 0; |
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_checksum = 0; |
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//checksum erro
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break; |
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}
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_step++; |
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_checksum = 0; |
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_payload_counter = 0; // prepare to receive payload
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break; |
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case 4://parsing body
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_checksum += data; |
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if (_payload_counter < sizeof(_buffer)) { |
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_buffer.bytes[_payload_counter] = data; |
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} |
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if (++_payload_counter == _payload_length) |
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_step++; |
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break;
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case 5://body checksum
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_step = 0; |
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if (_checksum != data){ |
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break; |
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} |
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parse_body (); |
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} |
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} |
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} |
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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/*
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Alexmos Serial controlled mount backend class |
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*/ |
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#ifndef __AP_MOUNT_ALEXMOS_H__ |
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#define __AP_MOUNT_ALEXMOS_H__ |
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#include <AP_Mount.h> |
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#include <AP_HAL.h> |
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#include <AP_Param.h> |
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#include <AP_Math.h> |
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#include <AP_GPS.h> |
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#include <AP_AHRS.h> |
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#include <AP_Mount_Backend.h> |
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//definition of the commands id for the Alexmos Serial Protocol
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#define CMD_READ_PARAMS 'R' |
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#define CMD_WRITE_PARAMS 'W' |
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#define CMD_REALTIME_DATA 'D' |
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#define CMD_BOARD_INFO 'V' |
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#define CMD_CALIB_ACC 'A' |
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#define CMD_CALIB_GYRO 'g' |
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#define CMD_CALIB_EXT_GAIN 'G' |
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#define CMD_USE_DEFAULTS 'F' |
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#define CMD_CALIB_POLES 'P' |
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#define CMD_RESET 'r' |
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#define CMD_HELPER_DATA 'H' |
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#define CMD_CALIB_OFFSET 'O' |
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#define CMD_CALIB_BAT 'B' |
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#define CMD_MOTORS_ON 'M' |
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#define CMD_MOTORS_OFF 'm' |
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#define CMD_CONTROL 'C' |
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#define CMD_TRIGGER_PIN 'T' |
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#define CMD_EXECUTE_MENU 'E' |
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#define CMD_GET_ANGLES 'I' |
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#define CMD_CONFIRM 'C' |
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// Board v3.x only
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#define CMD_BOARD_INFO_3 20 |
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#define CMD_READ_PARAMS_3 21 |
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#define CMD_WRITE_PARAMS_3 22 |
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#define CMD_REALTIME_DATA_3 23 |
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#define CMD_SELECT_IMU_3 24 |
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#define CMD_READ_PROFILE_NAMES 28 |
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#define CMD_WRITE_PROFILE_NAMES 29 |
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#define CMD_QUEUE_PARAMS_INFO_3 30 |
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#define CMD_SET_PARAMS_3 31 |
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#define CMD_SAVE_PARAMS_3 32 |
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#define CMD_READ_PARAMS_EXT 33 |
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#define CMD_WRITE_PARAMS_EXT 34 |
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#define CMD_AUTO_PID 35 |
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#define CMD_SERVO_OUT 36 |
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#define CMD_ERROR 255 |
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#define MODE_NO_CONTROL 0 |
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#define MODE_SPEED 1 |
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#define MODE_ANGLE 2 |
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#define MODE_SPEED_ANGLE 3 |
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#define MODE_RC 4 |
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#define SPEED 30 // degree/s2
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#define VALUE_TO_DEGREE(d) ((float)((d * 720) >> 15)) |
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#define DEGREE_TO_VALUE(d) ((int16_t)((float)(d)*(1.0f/0.02197265625f))) |
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#define DEGREE_PER_SEC_TO_VALUE(d) ((int16_t)((float)(d)*(1.0f/0.1220740379f))) |
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class AP_Mount_Alexmos : public AP_Mount_Backend |
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{ |
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public: |
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//constructor
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AP_Mount_Alexmos(AP_Mount &frontend, uint8_t instance): |
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AP_Mount_Backend(frontend, instance), |
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_initialised(false) |
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{} |
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// init - performs any required initialisation for this instance
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virtual void init (); |
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// update mount position - should be called periodically
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virtual void update(); |
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// has_pan_control - returns true if this mount can control it's pan (required for multicopters)
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virtual bool has_pan_control() const; |
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// set_mode - sets mount's mode
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virtual void set_mode(enum MAV_MOUNT_MODE mode) ; |
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// status_msg - called to allow mounts to send their status to GCS via MAVLink
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virtual void status_msg(mavlink_channel_t chan) ; |
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private: |
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void get_angles( ); |
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void set_motor(bool on); |
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void get_boardinfo(); |
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void control_axis(const Vector3f& angle , bool targets_in_degrees); |
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void read_params(uint8_t profile_id); |
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void write_params(); |
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bool get_realtimedata( Vector3f& angle); |
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//Alexmos Serial Protocol reading part implementation
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void send_command(uint8_t cmd, uint8_t* data, uint8_t size); |
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void parse_body (); |
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void read_incoming (); |
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//structure for the Serial Protocol
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// CMD_BOARD_INFO
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struct PACKED alexmos_version { |
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uint8_t _board_version; |
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uint16_t _firmware_version; |
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uint8_t debug_mode; |
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uint16_t _board_features; |
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}; |
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// CMD_GET_ANGLES
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struct PACKED alexmos_angles { |
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int16_t angle_roll; |
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int16_t rc_angle_roll; |
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int16_t rc_speed_roll; |
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int16_t angle_pitch; |
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int16_t rc_angle_pitch; |
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int16_t rc_speed_pitch; |
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int16_t angle_yaw; |
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int16_t rc_angle_yaw; |
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int16_t rc_speed_yaw; |
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}; |
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// CMD_READ_PARAMS
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struct PACKED alexmos_params { |
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uint8_t profile_id; |
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uint8_t roll_P; |
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uint8_t roll_I; |
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uint8_t roll_D; |
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uint8_t roll_power; |
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uint8_t roll_invert; |
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uint8_t roll_poles; |
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uint8_t pitch_P; |
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uint8_t pitch_I; |
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uint8_t pitch_D; |
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uint8_t pitch_power; |
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uint8_t pitch_invert; |
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uint8_t pitch_poles; |
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uint8_t yaw_P; |
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uint8_t yaw_I; |
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uint8_t yaw_D; |
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uint8_t yaw_power; |
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uint8_t yaw_invert; |
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uint8_t yaw_poles; |
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uint8_t acc_limiter; |
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int8_t ext_fc_gain_roll; |
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int8_t ext_fc_gain_pitch; |
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int16_t roll_rc_min_angle; |
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int16_t roll_rc_max_angle; |
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uint8_t roll_rc_mode; |
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uint8_t roll_rc_lpf; |
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uint8_t roll_rc_speed; |
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uint8_t roll_rc_follow; |
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int16_t pitch_rc_min_angle; |
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int16_t pitch_rc_max_angle; |
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uint8_t pitch_rc_mode; |
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uint8_t pitch_rc_lpf; |
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uint8_t pitch_rc_speed; |
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uint8_t pitch_rc_follow; |
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int16_t yaw_rc_min_angle; |
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int16_t yaw_rc_max_angle; |
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uint8_t yaw_rc_mode; |
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uint8_t yaw_rc_lpf; |
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uint8_t yaw_rc_speed; |
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uint8_t yaw_rc_follow; |
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uint8_t gyro_trust; |
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uint8_t use_model; |
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uint8_t pwm_freq; |
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uint8_t serial_speed; |
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int8_t rc_trim_roll; |
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int8_t rc_trim_pitch; |
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int8_t rc_trim_yaw; |
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uint8_t rc_deadband; |
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uint8_t rc_expo_rate; |
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uint8_t rc_virt_mode; |
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uint8_t rc_map_roll; |
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uint8_t rc_map_pitch;
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uint8_t rc_map_yaw; |
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uint8_t rc_map_cmd; |
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uint8_t rc_map_fc_roll; |
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uint8_t rc_map_fc_pitch; |
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uint8_t rc_mix_fc_roll; |
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uint8_t rc_mix_fc_pitch; |
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uint8_t follow_mode; |
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uint8_t follow_deadband; |
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uint8_t follow_expo_rate; |
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int8_t follow_offset_roll; |
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int8_t follow_offset_pitch; |
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int8_t follow_offset_yaw; |
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int8_t axis_top; |
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int8_t axis_right; |
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uint8_t gyro_lpf; |
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uint8_t gyro_sens; |
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uint8_t i2c_internal_pullups; |
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uint8_t sky_gyro_calib; |
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uint8_t rc_cmd_low; |
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uint8_t rc_cmd_mid; |
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uint8_t rc_cmd_high; |
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uint8_t menu_cmd_1; |
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uint8_t menu_cmd_2; |
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uint8_t menu_cmd_3; |
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uint8_t menu_cmd_4; |
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uint8_t menu_cmd_5; |
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uint8_t menu_cmd_long; |
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uint8_t output_roll; |
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uint8_t output_pitch; |
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uint8_t output_yaw; |
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int16_t bat_threshold_alarm; |
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int16_t bat_threshold_motors; |
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int16_t bat_comp_ref; |
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uint8_t beeper_modes; |
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uint8_t follow_roll_mix_start; |
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uint8_t follow_roll_mix_range; |
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uint8_t booster_power_roll; |
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uint8_t booster_power_pitch; |
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uint8_t booster_power_yaw; |
||||
|
||||
uint8_t follow_speed_roll; |
||||
uint8_t follow_speed_pitch; |
||||
uint8_t follow_speed_yaw; |
||||
|
||||
uint8_t frame_angle_from_motors; |
||||
|
||||
uint8_t cur_profile_id; |
||||
|
||||
}; |
||||
union PACKED { |
||||
alexmos_version version; |
||||
alexmos_angles angles; |
||||
alexmos_params params; |
||||
uint8_t bytes[]; |
||||
} _buffer,_current_parameters; |
||||
|
||||
AP_HAL::UARTDriver *_port; |
||||
bool _initialised; |
||||
|
||||
// result of the get_boardinfo
|
||||
uint8_t _board_version; |
||||
float _current_firmware_version; |
||||
uint8_t _firmware_beta_version; |
||||
bool _gimbal_3axis ; |
||||
bool _gimbal_bat_monitoring ; |
||||
|
||||
// keep the last _current_angle values
|
||||
Vector3f _current_angle; |
||||
|
||||
//CMD_READ_PARAMS has been called once
|
||||
bool _param_read_once; |
||||
|
||||
// Serial Protocol Variables
|
||||
uint8_t _checksum ; |
||||
uint8_t _step ; |
||||
uint8_t _command_id; |
||||
uint8_t _payload_length ; |
||||
uint8_t _payload_counter ; |
||||
|
||||
// confirmed that last command was ok
|
||||
bool _last_command_confirmed; |
||||
}; |
||||
|
||||
|
||||
#endif |
Loading…
Reference in new issue