ardupilot/libraries/AP_Mount/AP_Mount_SToRM32_serial.cpp

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#include "AP_Mount_SToRM32_serial.h"
#if HAL_MOUNT_STORM32SERIAL_ENABLED
#include <AP_HAL/AP_HAL.h>
#include <GCS_MAVLink/GCS_MAVLink.h>
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#include <GCS_MAVLink/include/mavlink/v2.0/checksum.h>
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// update mount position - should be called periodically
void AP_Mount_SToRM32_serial::update()
{
// exit immediately if not initialised
if (!_initialised) {
return;
}
read_incoming(); // read the incoming messages from the gimbal
// change to RC_TARGETING mode if RC input has changed
set_rctargeting_on_rcinput_change();
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// flag to trigger sending target angles to gimbal
bool resend_now = false;
// update based on mount mode
switch(get_mode()) {
// move mount to a "retracted" position. To-Do: remove support and replace with a relaxed mode?
case MAV_MOUNT_MODE_RETRACT: {
const Vector3f &target = _params.retract_angles.get();
mnt_target.angle_rad.set(target*DEG_TO_RAD, false);
mnt_target.target_type = MountTargetType::ANGLE;
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break;
}
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// move mount to a neutral position, typically pointing forward
case MAV_MOUNT_MODE_NEUTRAL: {
const Vector3f &target = _params.neutral_angles.get();
mnt_target.angle_rad.set(target*DEG_TO_RAD, false);
mnt_target.target_type = MountTargetType::ANGLE;
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break;
}
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// point to the angles given by a mavlink message
case MAV_MOUNT_MODE_MAVLINK_TARGETING:
// mnt_target should have already been filled in by set_angle_target() or set_rate_target()
if (mnt_target.target_type == MountTargetType::RATE) {
update_angle_target_from_rate(mnt_target.rate_rads, mnt_target.angle_rad);
}
resend_now = true;
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break;
// RC radio manual angle control, but with stabilization from the AHRS
case MAV_MOUNT_MODE_RC_TARGETING: {
// update targets using pilot's RC inputs
MountTarget rc_target;
get_rc_target(mnt_target.target_type, rc_target);
switch (mnt_target.target_type) {
case MountTargetType::ANGLE:
mnt_target.angle_rad = rc_target;
break;
case MountTargetType::RATE:
mnt_target.rate_rads = rc_target;
break;
}
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resend_now = true;
break;
}
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// point mount to a GPS point given by the mission planner
case MAV_MOUNT_MODE_GPS_POINT:
if (get_angle_target_to_roi(mnt_target.angle_rad)) {
mnt_target.target_type = MountTargetType::ANGLE;
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resend_now = true;
}
break;
// point mount to Home location
case MAV_MOUNT_MODE_HOME_LOCATION:
if (get_angle_target_to_home(mnt_target.angle_rad)) {
mnt_target.target_type = MountTargetType::ANGLE;
resend_now = true;
}
break;
// point mount to another vehicle
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case MAV_MOUNT_MODE_SYSID_TARGET:
if (get_angle_target_to_sysid(mnt_target.angle_rad)) {
mnt_target.target_type = MountTargetType::ANGLE;
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resend_now = true;
}
break;
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default:
// we do not know this mode so do nothing
break;
}
// resend target angles at least once per second
resend_now = resend_now || ((AP_HAL::millis() - _last_send) > AP_MOUNT_STORM32_SERIAL_RESEND_MS);
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if ((AP_HAL::millis() - _last_send) > AP_MOUNT_STORM32_SERIAL_RESEND_MS*2) {
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_reply_type = ReplyType_UNKNOWN;
}
if (can_send(resend_now)) {
if (resend_now) {
send_target_angles(mnt_target.angle_rad);
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get_angles();
_reply_type = ReplyType_ACK;
_reply_counter = 0;
_reply_length = get_reply_size(_reply_type);
} else {
get_angles();
_reply_type = ReplyType_DATA;
_reply_counter = 0;
_reply_length = get_reply_size(_reply_type);
}
}
}
// get attitude as a quaternion. returns true on success
bool AP_Mount_SToRM32_serial::get_attitude_quaternion(Quaternion& att_quat)
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{
att_quat.from_euler(radians(_current_angle.x * 0.01f), radians(_current_angle.y * 0.01f), radians(_current_angle.z * 0.01f));
return true;
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}
bool AP_Mount_SToRM32_serial::can_send(bool with_control) {
uint16_t required_tx = 1;
if (with_control) {
required_tx += sizeof(AP_Mount_SToRM32_serial::cmd_set_angles_struct);
}
return (_reply_type == ReplyType_UNKNOWN) && (_uart->txspace() >= required_tx);
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}
// send_target_angles
void AP_Mount_SToRM32_serial::send_target_angles(const MountTarget& angle_target_rad)
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{
static cmd_set_angles_struct cmd_set_angles_data = {
0xFA,
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0x0E,
0x11,
0, // pitch
0, // roll
0, // yaw
0, // flags
0, // type
0, // crc
};
// exit immediately if not initialised
if (!_initialised) {
return;
}
if ((size_t)_uart->txspace() < sizeof(cmd_set_angles_data)) {
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return;
}
// send CMD_SETANGLE (Note: reversed pitch and yaw)
cmd_set_angles_data.pitch = -degrees(angle_target_rad.pitch);
cmd_set_angles_data.roll = degrees(angle_target_rad.roll);
cmd_set_angles_data.yaw = -degrees(angle_target_rad.get_bf_yaw());
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uint8_t* buf = (uint8_t*)&cmd_set_angles_data;
cmd_set_angles_data.crc = crc_calculate(&buf[1], sizeof(cmd_set_angles_data)-3);
for (uint8_t i = 0; i != sizeof(cmd_set_angles_data) ; i++) {
_uart->write(buf[i]);
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}
// store time of send
_last_send = AP_HAL::millis();
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}
void AP_Mount_SToRM32_serial::get_angles() {
// exit immediately if not initialised
if (!_initialised) {
return;
}
if (_uart->txspace() < 1) {
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return;
}
_uart->write('d');
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};
uint8_t AP_Mount_SToRM32_serial::get_reply_size(ReplyType reply_type) {
switch (reply_type) {
case ReplyType_DATA:
return sizeof(SToRM32_reply_data_struct);
break;
case ReplyType_ACK:
return sizeof(SToRM32_reply_ack_struct);
break;
default:
return 0;
}
}
void AP_Mount_SToRM32_serial::read_incoming() {
uint8_t data;
int16_t numc;
numc = _uart->available();
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if (numc < 0 ) {
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return;
}
for (int16_t i = 0; i < numc; i++) { // Process bytes received
data = _uart->read();
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if (_reply_type == ReplyType_UNKNOWN) {
continue;
}
_buffer[_reply_counter++] = data;
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if (_reply_counter == _reply_length) {
parse_reply();
switch (_reply_type) {
case ReplyType_ACK:
_reply_type = ReplyType_DATA;
_reply_length = get_reply_size(_reply_type);
_reply_counter = 0;
break;
case ReplyType_DATA:
_reply_type = ReplyType_UNKNOWN;
_reply_length = get_reply_size(_reply_type);
_reply_counter = 0;
break;
default:
_reply_length = get_reply_size(_reply_type);
_reply_counter = 0;
break;
}
}
}
}
void AP_Mount_SToRM32_serial::parse_reply() {
uint16_t crc;
bool crc_ok;
switch (_reply_type) {
case ReplyType_DATA:
crc = crc_calculate(&_buffer[0], sizeof(_buffer.data) - 3);
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crc_ok = crc == _buffer.data.crc;
if (!crc_ok) {
break;
}
// Parse angles (Note: reversed pitch and yaw) to match ardupilot coordinate system
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_current_angle.x = _buffer.data.imu1_roll;
_current_angle.y = -_buffer.data.imu1_pitch;
_current_angle.z = -_buffer.data.imu1_yaw;
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break;
default:
break;
}
}
#endif // HAL_MOUNT_STORM32SERIAL_ENABLED