void ml_logger_default_write_manual_control(ml_logger_t* mll, mavlink_message_t* msg)
{
/**
int16_t x; ///< X-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to forward(1000)-backward(-1000) movement on a joystick and the pitch of a vehicle.
int16_t y; ///< Y-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to left(-1000)-right(1000) movement on a joystick and the roll of a vehicle.
int16_t z; ///< Z-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to a separate slider movement with maximum being 1000 and minimum being -1000 on a joystick and the thrust of a vehicle.
int16_t r; ///< R-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to a twisting of the joystick, with counter-clockwise being 1000 and clockwise being -1000, and the yaw of a vehicle.
uint16_t buttons; ///< A bitfield corresponding to the joystick buttons' current state, 1 for pressed, 0 for released. The lowest bit corresponds to Button 1.
uint8_t target; ///< The system to be controlled.
**/
/**
x = roll [-600,600]
y = pitch [-600,600]
z = yaw [-2000,2000]
r = thrust [0,1000]
**/
if (msg->msgid == MAVLINK_MSG_ID_MANUAL_CONTROL)
{
mavlink_manual_control_t mc;
mavlink_msg_manual_control_decode(msg, &mc);
fprintf(mll->files.manual_control.fs, "%12" PRIu64 " %5d %5d %5d %5d %5d %3d\n",
utils_us_since_epoch(),
mc.x,
mc.y,
mc.z,
mc.r,
mc.buttons,
mc.target
);
fflush(mll->files.manual_control.fs);
}
}
void *MavlinkReceiveTask(void *ptr) {
MavlinkStruct *Mavlink = (MavlinkStruct *) ptr;
AttitudeData *AttitudeDesire = Mavlink->AttitudeDesire;
AttData Data, Speed;
double Pitch, Roll, Yaw, Elevation;
mavlink_message_t msg;
mavlink_status_t status;
mavlink_manual_control_t man_control;
socklen_t fromlen;
ssize_t recsize;
uint8_t buf[BUFFER_LENGTH];
int i = 0;
printf("%s : Mavlink Receive démarré\n", __FUNCTION__);
pthread_barrier_wait(&(MavlinkStartBarrier));
while (MavlinkActivated) {
sem_wait(&MavlinkReceiveTimerSem);
if (MavlinkActivated == 0)
break;
memset(buf, 0, BUFFER_LENGTH);
recsize = recvfrom(Mavlink->sock, (void *)buf, BUFFER_LENGTH, 0, (struct sockaddr *)&Mavlink->gcAddr, &fromlen);
if (recsize > 0) {
// Something received - print out all bytes and parse packet
for (i = 0; i < recsize; ++i) {
if (mavlink_parse_char(MAVLINK_COMM_0, buf[i], &msg, &status)) {
// Packet received
}
}
if (msg.msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) {
mavlink_msg_manual_control_decode(&msg, &man_control);
Pitch = -((double)man_control.y/1000.0)*PITCH_MAX*M_PI/180.0;
Roll = ((double)man_control.x/1000.0)*ROLL_MAX*M_PI/180.0;
Yaw = -((double)man_control.r/1000.0)*YAW_MAX*M_PI/180.0;
Elevation = HEIGHT_MAX*((double)man_control.z/1000.0);
Speed.Pitch = (Pitch - Data.Pitch)/TS;
Speed.Roll = (Roll - Data.Roll)/TS;
Speed.Yaw = (Yaw - Data.Yaw)/TS;
Speed.Elevation = (Elevation - Data.Elevation)/TS;
Data.Pitch = Pitch;
Data.Roll = Roll;
Data.Yaw = Yaw;
Data.Elevation = Elevation;
pthread_spin_lock(&(AttitudeDesire->AttitudeLock));
memcpy((void *) &(AttitudeDesire->Data), (void *) &Data, sizeof(AttData));
memcpy((void *) &(AttitudeDesire->Speed), (void *) &Speed, sizeof(AttData));
AttitudeDesire->Throttle = (float)man_control.z/1000;
pthread_spin_unlock(&(AttitudeDesire->AttitudeLock));
} else { // Un message non attendu a ete recu
}
}
}
printf("%s : Mavlink Receive Arrêté\n", __FUNCTION__);
pthread_exit(NULL);
}
void
MavlinkReceiver::handle_message_manual_control(mavlink_message_t *msg)
{
mavlink_manual_control_t man;
mavlink_msg_manual_control_decode(msg, &man);
/* rc channels */
{
struct rc_channels_s rc;
memset(&rc, 0, sizeof(rc));
rc.timestamp = hrt_absolute_time();
rc.chan_count = 4;
rc.chan[0].scaled = man.x / 1000.0f;
rc.chan[1].scaled = man.y / 1000.0f;
rc.chan[2].scaled = man.r / 1000.0f;
rc.chan[3].scaled = man.z / 1000.0f;
if (_rc_pub < 0) {
_rc_pub = orb_advertise(ORB_ID(rc_channels), &rc);
} else {
orb_publish(ORB_ID(rc_channels), _rc_pub, &rc);
}
}
/* manual control */
{
struct manual_control_setpoint_s manual;
memset(&manual, 0, sizeof(manual));
/* get a copy first, to prevent altering values that are not sent by the mavlink command */
orb_copy(ORB_ID(manual_control_setpoint), _manual_sub, &manual);
manual.timestamp = hrt_absolute_time();
manual.roll = man.x / 1000.0f;
manual.pitch = man.y / 1000.0f;
manual.yaw = man.r / 1000.0f;
manual.throttle = man.z / 1000.0f;
if (_manual_pub < 0) {
_manual_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual);
} else {
orb_publish(ORB_ID(manual_control_setpoint), _manual_pub, &manual);
}
}
}
static void joystick_telemetry_parse_msg(joystick_t* joystick, uint32_t sysid, mavlink_message_t* msg)
{
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
if ((uint8_t)packet.target == (uint8_t)sysid)
{
joystick->channels.x = packet.x / 1000.0f;
joystick->channels.y = packet.y / 1000.0f;
joystick->channels.r = packet.r / 1000.0f;
joystick->channels.z = packet.z / 1000.0f;
joystick_button_mask(joystick, packet.buttons);
}
}
void handle_manual_control(const mavlink_message_t *msg, uint8_t sysid, uint8_t compid) {
mavlink_manual_control_t manual_control;
mavlink_msg_manual_control_decode(msg, &manual_control);
auto manual_control_msg = boost::make_shared<mavros_msgs::ManualControl>();
manual_control_msg->header.stamp = ros::Time::now();
manual_control_msg->x = (manual_control.x / 1000.0);
manual_control_msg->y = (manual_control.y / 1000.0);
manual_control_msg->z = (manual_control.z / 1000.0);
manual_control_msg->r = (manual_control.r / 1000.0);
manual_control_msg->buttons = manual_control.buttons;
control_pub.publish(manual_control_msg);
}
void GCS_MAVLINK_Rover::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
case MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE:
{
// allow override of RC channel values for HIL
// or for complete GCS control of switch position
// and RC PWM values.
if (msg->sysid != rover.g.sysid_my_gcs) { // Only accept control from our gcs
break;
}
uint32_t tnow = AP_HAL::millis();
mavlink_rc_channels_override_t packet;
mavlink_msg_rc_channels_override_decode(msg, &packet);
RC_Channels::set_override(0, packet.chan1_raw, tnow);
RC_Channels::set_override(1, packet.chan2_raw, tnow);
RC_Channels::set_override(2, packet.chan3_raw, tnow);
RC_Channels::set_override(3, packet.chan4_raw, tnow);
RC_Channels::set_override(4, packet.chan5_raw, tnow);
RC_Channels::set_override(5, packet.chan6_raw, tnow);
RC_Channels::set_override(6, packet.chan7_raw, tnow);
RC_Channels::set_override(7, packet.chan8_raw, tnow);
break;
}
case MAVLINK_MSG_ID_MANUAL_CONTROL:
{
if (msg->sysid != rover.g.sysid_my_gcs) { // Only accept control from our gcs
break;
}
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
if (packet.target != rover.g.sysid_this_mav) {
break; // only accept control aimed at us
}
uint32_t tnow = AP_HAL::millis();
const int16_t roll = (packet.y == INT16_MAX) ? 0 : rover.channel_steer->get_radio_min() + (rover.channel_steer->get_radio_max() - rover.channel_steer->get_radio_min()) * (packet.y + 1000) / 2000.0f;
const int16_t throttle = (packet.z == INT16_MAX) ? 0 : rover.channel_throttle->get_radio_min() + (rover.channel_throttle->get_radio_max() - rover.channel_throttle->get_radio_min()) * (packet.z + 1000) / 2000.0f;
RC_Channels::set_override(uint8_t(rover.rcmap.roll() - 1), roll, tnow);
RC_Channels::set_override(uint8_t(rover.rcmap.throttle() - 1), throttle, tnow);
break;
}
case MAVLINK_MSG_ID_HEARTBEAT:
{
// We keep track of the last time we received a heartbeat from our GCS for failsafe purposes
if (msg->sysid != rover.g.sysid_my_gcs) {
break;
}
rover.last_heartbeat_ms = AP_HAL::millis();
rover.failsafe_trigger(FAILSAFE_EVENT_GCS, false);
break;
}
case MAVLINK_MSG_ID_SET_ATTITUDE_TARGET: // MAV ID: 82
{
// decode packet
mavlink_set_attitude_target_t packet;
mavlink_msg_set_attitude_target_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// ensure type_mask specifies to use thrust
if ((packet.type_mask & MAVLINK_SET_ATT_TYPE_MASK_THROTTLE_IGNORE) != 0) {
break;
}
// convert thrust to ground speed
packet.thrust = constrain_float(packet.thrust, -1.0f, 1.0f);
const float target_speed = rover.control_mode->get_speed_default() * packet.thrust;
// if the body_yaw_rate field is ignored, convert quaternion to heading
if ((packet.type_mask & MAVLINK_SET_ATT_TYPE_MASK_YAW_RATE_IGNORE) != 0) {
// convert quaternion to heading
float target_heading_cd = degrees(Quaternion(packet.q[0], packet.q[1], packet.q[2], packet.q[3]).get_euler_yaw()) * 100.0f;
rover.mode_guided.set_desired_heading_and_speed(target_heading_cd, target_speed);
} else {
// use body_yaw_rate field
rover.mode_guided.set_desired_turn_rate_and_speed((RAD_TO_DEG * packet.body_yaw_rate) * 100.0f, target_speed);
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED: // MAV ID: 84
{
// decode packet
mavlink_set_position_target_local_ned_t packet;
mavlink_msg_set_position_target_local_ned_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_LOCAL_NED &&
packet.coordinate_frame != MAV_FRAME_LOCAL_OFFSET_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_OFFSET_NED) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
// prepare target position
Location target_loc = rover.current_loc;
if (!pos_ignore) {
switch (packet.coordinate_frame) {
case MAV_FRAME_BODY_NED:
case MAV_FRAME_BODY_OFFSET_NED: {
// rotate from body-frame to NE frame
const float ne_x = packet.x * rover.ahrs.cos_yaw() - packet.y * rover.ahrs.sin_yaw();
const float ne_y = packet.x * rover.ahrs.sin_yaw() + packet.y * rover.ahrs.cos_yaw();
// add offset to current location
location_offset(target_loc, ne_x, ne_y);
}
break;
case MAV_FRAME_LOCAL_OFFSET_NED:
// add offset to current location
location_offset(target_loc, packet.x, packet.y);
break;
default:
// MAV_FRAME_LOCAL_NED interpret as an offset from home
target_loc = rover.ahrs.get_home();
location_offset(target_loc, packet.x, packet.y);
break;
}
}
float target_speed = 0.0f;
float target_yaw_cd = 0.0f;
// consume velocity and convert to target speed and heading
if (!vel_ignore) {
const float speed_max = rover.control_mode->get_speed_default();
// convert vector length into a speed
target_speed = constrain_float(safe_sqrt(sq(packet.vx) + sq(packet.vy)), -speed_max, speed_max);
// convert vector direction to target yaw
target_yaw_cd = degrees(atan2f(packet.vy, packet.vx)) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw heading
if (!yaw_ignore) {
target_yaw_cd = ToDeg(packet.yaw) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw rate
float target_turn_rate_cds = 0.0f;
if (!yaw_rate_ignore) {
target_turn_rate_cds = ToDeg(packet.yaw_rate) * 100.0f;
}
// handling case when both velocity and either yaw or yaw-rate are provided
// by default, we consider that the rover will drive forward
float speed_dir = 1.0f;
if (!vel_ignore && (!yaw_ignore || !yaw_rate_ignore)) {
// Note: we are using the x-axis velocity to determine direction even though
// the frame may have been provided in MAV_FRAME_LOCAL_OFFSET_NED or MAV_FRAME_LOCAL_NED
if (is_negative(packet.vx)) {
speed_dir = -1.0f;
}
}
// set guided mode targets
if (!pos_ignore) {
// consume position target
rover.mode_guided.set_desired_location(target_loc);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume velocity and turn rate
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume just target heading (probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, 0.0f);
} else if (pos_ignore && vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume just turn rate(probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, 0.0f);
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT: // MAV ID: 86
{
// decode packet
mavlink_set_position_target_global_int_t packet;
mavlink_msg_set_position_target_global_int_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_GLOBAL &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_INT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_RELATIVE_ALT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_RELATIVE_ALT_INT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_TERRAIN_ALT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_TERRAIN_ALT_INT) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
// prepare target position
Location target_loc = rover.current_loc;
if (!pos_ignore) {
// sanity check location
if (!check_latlng(packet.lat_int, packet.lon_int)) {
// result = MAV_RESULT_FAILED;
break;
}
target_loc.lat = packet.lat_int;
target_loc.lng = packet.lon_int;
}
float target_speed = 0.0f;
float target_yaw_cd = 0.0f;
// consume velocity and convert to target speed and heading
if (!vel_ignore) {
const float speed_max = rover.control_mode->get_speed_default();
// convert vector length into a speed
target_speed = constrain_float(safe_sqrt(sq(packet.vx) + sq(packet.vy)), -speed_max, speed_max);
// convert vector direction to target yaw
target_yaw_cd = degrees(atan2f(packet.vy, packet.vx)) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw heading
if (!yaw_ignore) {
target_yaw_cd = ToDeg(packet.yaw) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw rate
float target_turn_rate_cds = 0.0f;
if (!yaw_rate_ignore) {
target_turn_rate_cds = ToDeg(packet.yaw_rate) * 100.0f;
}
// handling case when both velocity and either yaw or yaw-rate are provided
// by default, we consider that the rover will drive forward
float speed_dir = 1.0f;
if (!vel_ignore && (!yaw_ignore || !yaw_rate_ignore)) {
// Note: we are using the x-axis velocity to determine direction even though
// the frame is provided in MAV_FRAME_GLOBAL_xxx
if (is_negative(packet.vx)) {
speed_dir = -1.0f;
}
}
// set guided mode targets
if (!pos_ignore) {
// consume position target
rover.mode_guided.set_desired_location(target_loc);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume velocity and turn rate
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume just target heading (probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, 0.0f);
} else if (pos_ignore && vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume just turn rate(probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, 0.0f);
}
break;
}
#if HIL_MODE != HIL_MODE_DISABLED
case MAVLINK_MSG_ID_HIL_STATE:
{
mavlink_hil_state_t packet;
mavlink_msg_hil_state_decode(msg, &packet);
// sanity check location
if (!check_latlng(packet.lat, packet.lon)) {
break;
}
// set gps hil sensor
Location loc;
loc.lat = packet.lat;
loc.lng = packet.lon;
loc.alt = packet.alt/10;
Vector3f vel(packet.vx, packet.vy, packet.vz);
vel *= 0.01f;
gps.setHIL(0, AP_GPS::GPS_OK_FIX_3D,
packet.time_usec/1000,
loc, vel, 10, 0);
// rad/sec
Vector3f gyros;
gyros.x = packet.rollspeed;
gyros.y = packet.pitchspeed;
gyros.z = packet.yawspeed;
// m/s/s
Vector3f accels;
accels.x = packet.xacc * (GRAVITY_MSS/1000.0f);
accels.y = packet.yacc * (GRAVITY_MSS/1000.0f);
accels.z = packet.zacc * (GRAVITY_MSS/1000.0f);
ins.set_gyro(0, gyros);
ins.set_accel(0, accels);
compass.setHIL(0, packet.roll, packet.pitch, packet.yaw);
compass.setHIL(1, packet.roll, packet.pitch, packet.yaw);
break;
}
#endif // HIL_MODE
#if MOUNT == ENABLED
// deprecated. Use MAV_CMD_DO_MOUNT_CONFIGURE
case MAVLINK_MSG_ID_MOUNT_CONFIGURE:
{
rover.camera_mount.configure_msg(msg);
break;
}
// deprecated. Use MAV_CMD_DO_MOUNT_CONTROL
case MAVLINK_MSG_ID_MOUNT_CONTROL:
{
rover.camera_mount.control_msg(msg);
break;
}
#endif // MOUNT == ENABLED
case MAVLINK_MSG_ID_RADIO:
case MAVLINK_MSG_ID_RADIO_STATUS:
{
handle_radio_status(msg, rover.DataFlash, rover.should_log(MASK_LOG_PM));
break;
}
// send or receive fence points with GCS
case MAVLINK_MSG_ID_FENCE_POINT: // MAV ID: 160
case MAVLINK_MSG_ID_FENCE_FETCH_POINT:
rover.g2.fence.handle_msg(*this, msg);
break;
case MAVLINK_MSG_ID_DISTANCE_SENSOR:
rover.rangefinder.handle_msg(msg);
rover.g2.proximity.handle_msg(msg);
break;
default:
handle_common_message(msg);
break;
} // end switch
} // end handle mavlink
void GCS_MAVLINK::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
// If we are currently operating as a proxy for a remote,
// alas we have to look inside each packet to see if its for us or for the remote
case MAVLINK_MSG_ID_REQUEST_DATA_STREAM:
{
handle_request_data_stream(msg, true);
break;
}
case MAVLINK_MSG_ID_PARAM_REQUEST_LIST:
{
handle_param_request_list(msg);
break;
}
case MAVLINK_MSG_ID_PARAM_REQUEST_READ:
{
handle_param_request_read(msg);
break;
}
case MAVLINK_MSG_ID_PARAM_SET:
{
handle_param_set(msg, NULL);
break;
}
case MAVLINK_MSG_ID_HEARTBEAT:
break;
case MAVLINK_MSG_ID_COMMAND_LONG:
{
// decode
mavlink_command_long_t packet;
mavlink_msg_command_long_decode(msg, &packet);
uint8_t result = MAV_RESULT_UNSUPPORTED;
// do command
send_text_P(SEVERITY_LOW,PSTR("command received: "));
switch(packet.command) {
case MAV_CMD_PREFLIGHT_CALIBRATION:
{
if (is_equal(packet.param1,1.0f)) {
tracker.ins.init_gyro();
if (tracker.ins.gyro_calibrated_ok_all()) {
tracker.ahrs.reset_gyro_drift();
result = MAV_RESULT_ACCEPTED;
} else {
result = MAV_RESULT_FAILED;
}
}
if (is_equal(packet.param3,1.0f)) {
tracker.init_barometer();
// zero the altitude difference on next baro update
tracker.nav_status.need_altitude_calibration = true;
}
if (is_equal(packet.param4,1.0f)) {
// Cant trim radio
} else if (is_equal(packet.param5,1.0f)) {
float trim_roll, trim_pitch;
AP_InertialSensor_UserInteract_MAVLink interact(this);
if(tracker.ins.calibrate_accel(&interact, trim_roll, trim_pitch)) {
// reset ahrs's trim to suggested values from calibration routine
tracker.ahrs.set_trim(Vector3f(trim_roll, trim_pitch, 0));
}
} else if (is_equal(packet.param5,2.0f)) {
// accel trim
float trim_roll, trim_pitch;
if(tracker.ins.calibrate_trim(trim_roll, trim_pitch)) {
// reset ahrs's trim to suggested values from calibration routine
tracker.ahrs.set_trim(Vector3f(trim_roll, trim_pitch, 0));
result = MAV_RESULT_ACCEPTED;
} else {
result = MAV_RESULT_FAILED;
}
}
result = MAV_RESULT_ACCEPTED;
break;
}
case MAV_CMD_COMPONENT_ARM_DISARM:
if (packet.target_component == MAV_COMP_ID_SYSTEM_CONTROL) {
if (is_equal(packet.param1,1.0f)) {
tracker.arm_servos();
result = MAV_RESULT_ACCEPTED;
} else if (is_zero(packet.param1)) {
tracker.disarm_servos();
result = MAV_RESULT_ACCEPTED;
} else {
result = MAV_RESULT_UNSUPPORTED;
}
} else {
result = MAV_RESULT_UNSUPPORTED;
}
break;
case MAV_CMD_DO_SET_MODE:
switch ((uint16_t)packet.param1) {
case MAV_MODE_MANUAL_ARMED:
case MAV_MODE_MANUAL_DISARMED:
tracker.set_mode(MANUAL);
result = MAV_RESULT_ACCEPTED;
break;
case MAV_MODE_AUTO_ARMED:
case MAV_MODE_AUTO_DISARMED:
tracker.set_mode(AUTO);
result = MAV_RESULT_ACCEPTED;
break;
default:
result = MAV_RESULT_UNSUPPORTED;
}
break;
case MAV_CMD_DO_SET_SERVO:
if (tracker.servo_test_set_servo(packet.param1, packet.param2)) {
result = MAV_RESULT_ACCEPTED;
}
break;
// mavproxy/mavutil sends this when auto command is entered
case MAV_CMD_MISSION_START:
tracker.set_mode(AUTO);
result = MAV_RESULT_ACCEPTED;
break;
case MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN:
{
if (is_equal(packet.param1,1.0f) || is_equal(packet.param1,3.0f)) {
// when packet.param1 == 3 we reboot to hold in bootloader
hal.scheduler->reboot(is_equal(packet.param1,3.0f));
result = MAV_RESULT_ACCEPTED;
}
break;
}
case MAV_CMD_REQUEST_AUTOPILOT_CAPABILITIES: {
if (is_equal(packet.param1,1.0f)) {
tracker.gcs[chan-MAVLINK_COMM_0].send_autopilot_version();
result = MAV_RESULT_ACCEPTED;
}
break;
}
default:
break;
}
mavlink_msg_command_ack_send(
chan,
packet.command,
result);
break;
}
// When mavproxy 'wp sethome'
case MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST:
{
// decode
mavlink_mission_write_partial_list_t packet;
mavlink_msg_mission_write_partial_list_decode(msg, &packet);
if (packet.start_index == 0)
{
// New home at wp index 0. Ask for it
waypoint_receiving = true;
waypoint_request_i = 0;
waypoint_request_last = 0;
send_message(MSG_NEXT_WAYPOINT);
waypoint_receiving = true;
}
break;
}
// XXX receive a WP from GCS and store in EEPROM if it is HOME
case MAVLINK_MSG_ID_MISSION_ITEM:
{
// decode
mavlink_mission_item_t packet;
uint8_t result = MAV_MISSION_ACCEPTED;
mavlink_msg_mission_item_decode(msg, &packet);
struct Location tell_command = {};
switch (packet.frame)
{
case MAV_FRAME_MISSION:
case MAV_FRAME_GLOBAL:
{
tell_command.lat = 1.0e7f*packet.x; // in as DD converted to * t7
tell_command.lng = 1.0e7f*packet.y; // in as DD converted to * t7
tell_command.alt = packet.z*1.0e2f; // in as m converted to cm
tell_command.options = 0; // absolute altitude
break;
}
#ifdef MAV_FRAME_LOCAL_NED
case MAV_FRAME_LOCAL_NED: // local (relative to home position)
{
tell_command.lat = 1.0e7f*ToDeg(packet.x/
(RADIUS_OF_EARTH*cosf(ToRad(home.lat/1.0e7f)))) + home.lat;
tell_command.lng = 1.0e7f*ToDeg(packet.y/RADIUS_OF_EARTH) + home.lng;
tell_command.alt = -packet.z*1.0e2f;
tell_command.options = MASK_OPTIONS_RELATIVE_ALT;
break;
}
#endif
#ifdef MAV_FRAME_LOCAL
case MAV_FRAME_LOCAL: // local (relative to home position)
{
tell_command.lat = 1.0e7f*ToDeg(packet.x/
(RADIUS_OF_EARTH*cosf(ToRad(home.lat/1.0e7f)))) + home.lat;
tell_command.lng = 1.0e7f*ToDeg(packet.y/RADIUS_OF_EARTH) + home.lng;
tell_command.alt = packet.z*1.0e2f;
tell_command.options = MASK_OPTIONS_RELATIVE_ALT;
break;
}
#endif
case MAV_FRAME_GLOBAL_RELATIVE_ALT: // absolute lat/lng, relative altitude
{
tell_command.lat = 1.0e7f * packet.x; // in as DD converted to * t7
tell_command.lng = 1.0e7f * packet.y; // in as DD converted to * t7
tell_command.alt = packet.z * 1.0e2f;
tell_command.options = MASK_OPTIONS_RELATIVE_ALT; // store altitude relative!! Always!!
break;
}
default:
result = MAV_MISSION_UNSUPPORTED_FRAME;
break;
}
if (result != MAV_MISSION_ACCEPTED) goto mission_failed;
// Check if receiving waypoints (mission upload expected)
if (!waypoint_receiving) {
result = MAV_MISSION_ERROR;
goto mission_failed;
}
// check if this is the HOME wp
if (packet.seq == 0) {
tracker.set_home(tell_command); // New home in EEPROM
send_text_P(SEVERITY_LOW,PSTR("new HOME received"));
waypoint_receiving = false;
}
mission_failed:
// we are rejecting the mission/waypoint
mavlink_msg_mission_ack_send(
chan,
msg->sysid,
msg->compid,
result);
break;
}
case MAVLINK_MSG_ID_MANUAL_CONTROL:
{
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
tracker.tracking_manual_control(packet);
break;
}
case MAVLINK_MSG_ID_GLOBAL_POSITION_INT:
{
// decode
mavlink_global_position_int_t packet;
mavlink_msg_global_position_int_decode(msg, &packet);
tracker.tracking_update_position(packet);
break;
}
case MAVLINK_MSG_ID_SCALED_PRESSURE:
{
// decode
mavlink_scaled_pressure_t packet;
mavlink_msg_scaled_pressure_decode(msg, &packet);
tracker.tracking_update_pressure(packet);
break;
}
case MAVLINK_MSG_ID_SET_MODE:
{
handle_set_mode(msg, FUNCTOR_BIND(&tracker, &Tracker::mavlink_set_mode, bool, uint8_t));
break;
}
#if HAL_CPU_CLASS > HAL_CPU_CLASS_16
case MAVLINK_MSG_ID_SERIAL_CONTROL:
handle_serial_control(msg, tracker.gps);
break;
case MAVLINK_MSG_ID_GPS_INJECT_DATA:
handle_gps_inject(msg, tracker.gps);
break;
#endif
case MAVLINK_MSG_ID_AUTOPILOT_VERSION_REQUEST:
tracker.gcs[chan-MAVLINK_COMM_0].send_autopilot_version();
break;
} // end switch
} // end handle mavlink
void GCS_MAVLINK_Tracker::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
case MAVLINK_MSG_ID_HEARTBEAT:
break;
// When mavproxy 'wp sethome'
case MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST:
{
// decode
mavlink_mission_write_partial_list_t packet;
mavlink_msg_mission_write_partial_list_decode(msg, &packet);
if (packet.start_index == 0)
{
// New home at wp index 0. Ask for it
waypoint_receiving = true;
waypoint_request_i = 0;
waypoint_request_last = 0;
send_message(MSG_NEXT_WAYPOINT);
}
break;
}
// XXX receive a WP from GCS and store in EEPROM if it is HOME
case MAVLINK_MSG_ID_MISSION_ITEM:
{
// decode
mavlink_mission_item_t packet;
MAV_MISSION_RESULT result = MAV_MISSION_ACCEPTED;
mavlink_msg_mission_item_decode(msg, &packet);
struct Location tell_command = {};
switch (packet.frame)
{
case MAV_FRAME_MISSION:
case MAV_FRAME_GLOBAL:
{
tell_command.lat = 1.0e7f*packet.x; // in as DD converted to * t7
tell_command.lng = 1.0e7f*packet.y; // in as DD converted to * t7
tell_command.alt = packet.z*1.0e2f; // in as m converted to cm
tell_command.options = 0; // absolute altitude
break;
}
#ifdef MAV_FRAME_LOCAL_NED
case MAV_FRAME_LOCAL_NED: // local (relative to home position)
{
tell_command.lat = 1.0e7f*ToDeg(packet.x/
(RADIUS_OF_EARTH*cosf(ToRad(home.lat/1.0e7f)))) + home.lat;
tell_command.lng = 1.0e7f*ToDeg(packet.y/RADIUS_OF_EARTH) + home.lng;
tell_command.alt = -packet.z*1.0e2f;
tell_command.options = MASK_OPTIONS_RELATIVE_ALT;
break;
}
#endif
#ifdef MAV_FRAME_LOCAL
case MAV_FRAME_LOCAL: // local (relative to home position)
{
tell_command.lat = 1.0e7f*ToDeg(packet.x/
(RADIUS_OF_EARTH*cosf(ToRad(home.lat/1.0e7f)))) + home.lat;
tell_command.lng = 1.0e7f*ToDeg(packet.y/RADIUS_OF_EARTH) + home.lng;
tell_command.alt = packet.z*1.0e2f;
tell_command.options = MASK_OPTIONS_RELATIVE_ALT;
break;
}
#endif
case MAV_FRAME_GLOBAL_RELATIVE_ALT: // absolute lat/lng, relative altitude
{
tell_command.lat = 1.0e7f * packet.x; // in as DD converted to * t7
tell_command.lng = 1.0e7f * packet.y; // in as DD converted to * t7
tell_command.alt = packet.z * 1.0e2f;
tell_command.options = MASK_OPTIONS_RELATIVE_ALT; // store altitude relative!! Always!!
break;
}
default:
result = MAV_MISSION_UNSUPPORTED_FRAME;
break;
}
if (result != MAV_MISSION_ACCEPTED) goto mission_failed;
// Check if receiving waypoints (mission upload expected)
if (!waypoint_receiving) {
result = MAV_MISSION_ERROR;
goto mission_failed;
}
// check if this is the HOME wp
if (packet.seq == 0) {
tracker.set_home(tell_command); // New home in EEPROM
send_text(MAV_SEVERITY_INFO,"New HOME received");
waypoint_receiving = false;
}
mission_failed:
// we are rejecting the mission/waypoint
mavlink_msg_mission_ack_send(
chan,
msg->sysid,
msg->compid,
result,
MAV_MISSION_TYPE_MISSION);
break;
}
case MAVLINK_MSG_ID_MANUAL_CONTROL:
{
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
tracker.tracking_manual_control(packet);
break;
}
case MAVLINK_MSG_ID_GLOBAL_POSITION_INT:
{
// decode
mavlink_global_position_int_t packet;
mavlink_msg_global_position_int_decode(msg, &packet);
tracker.tracking_update_position(packet);
break;
}
case MAVLINK_MSG_ID_SCALED_PRESSURE:
{
// decode
mavlink_scaled_pressure_t packet;
mavlink_msg_scaled_pressure_decode(msg, &packet);
tracker.tracking_update_pressure(packet);
break;
}
default:
handle_common_message(msg);
break;
} // end switch
} // end handle mavlink
void GCS_MAVLINK_Plane::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
#if GEOFENCE_ENABLED == ENABLED
// receive a fence point from GCS and store in EEPROM
case MAVLINK_MSG_ID_FENCE_POINT: {
mavlink_fence_point_t packet;
mavlink_msg_fence_point_decode(msg, &packet);
if (plane.g.fence_action != FENCE_ACTION_NONE) {
send_text(MAV_SEVERITY_WARNING,"Fencing must be disabled");
} else if (packet.count != plane.g.fence_total) {
send_text(MAV_SEVERITY_WARNING,"Bad fence point");
} else if (!check_latlng(packet.lat,packet.lng)) {
send_text(MAV_SEVERITY_WARNING,"Invalid fence point, lat or lng too large");
} else {
plane.set_fence_point_with_index(Vector2l(packet.lat*1.0e7f, packet.lng*1.0e7f), packet.idx);
}
break;
}
// send a fence point to GCS
case MAVLINK_MSG_ID_FENCE_FETCH_POINT: {
mavlink_fence_fetch_point_t packet;
mavlink_msg_fence_fetch_point_decode(msg, &packet);
if (packet.idx >= plane.g.fence_total) {
send_text(MAV_SEVERITY_WARNING,"Bad fence point");
} else {
Vector2l point = plane.get_fence_point_with_index(packet.idx);
mavlink_msg_fence_point_send_buf(msg, chan, msg->sysid, msg->compid, packet.idx, plane.g.fence_total,
point.x*1.0e-7f, point.y*1.0e-7f);
}
break;
}
#endif // GEOFENCE_ENABLED
case MAVLINK_MSG_ID_MANUAL_CONTROL:
{
if (msg->sysid != plane.g.sysid_my_gcs) {
break; // only accept control from our gcs
}
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
if (packet.target != plane.g.sysid_this_mav) {
break; // only accept messages aimed at us
}
uint32_t tnow = AP_HAL::millis();
manual_override(plane.channel_roll, packet.y, 1000, 2000, tnow);
manual_override(plane.channel_pitch, packet.x, 1000, 2000, tnow, true);
manual_override(plane.channel_throttle, packet.z, 0, 1000, tnow);
manual_override(plane.channel_rudder, packet.r, 1000, 2000, tnow);
// a manual control message is considered to be a 'heartbeat' from the ground station for failsafe purposes
plane.failsafe.last_heartbeat_ms = tnow;
break;
}
case MAVLINK_MSG_ID_HEARTBEAT:
{
// We keep track of the last time we received a heartbeat from
// our GCS for failsafe purposes
if (msg->sysid != plane.g.sysid_my_gcs) break;
plane.failsafe.last_heartbeat_ms = AP_HAL::millis();
break;
}
case MAVLINK_MSG_ID_HIL_STATE:
{
#if HIL_SUPPORT
if (plane.g.hil_mode != 1) {
break;
}
mavlink_hil_state_t packet;
mavlink_msg_hil_state_decode(msg, &packet);
// sanity check location
if (!check_latlng(packet.lat, packet.lon)) {
break;
}
last_hil_state = packet;
// set gps hil sensor
const Location loc{packet.lat, packet.lon, packet.alt/10, Location::AltFrame::ABSOLUTE};
Vector3f vel(packet.vx, packet.vy, packet.vz);
vel *= 0.01f;
// setup airspeed pressure based on 3D speed, no wind
plane.airspeed.setHIL(sq(vel.length()) / 2.0f + 2013);
plane.gps.setHIL(0, AP_GPS::GPS_OK_FIX_3D,
packet.time_usec/1000,
loc, vel, 10, 0);
// rad/sec
Vector3f gyros;
gyros.x = packet.rollspeed;
gyros.y = packet.pitchspeed;
gyros.z = packet.yawspeed;
// m/s/s
Vector3f accels;
accels.x = packet.xacc * GRAVITY_MSS*0.001f;
accels.y = packet.yacc * GRAVITY_MSS*0.001f;
accels.z = packet.zacc * GRAVITY_MSS*0.001f;
plane.ins.set_gyro(0, gyros);
plane.ins.set_accel(0, accels);
plane.barometer.setHIL(packet.alt*0.001f);
plane.compass.setHIL(0, packet.roll, packet.pitch, packet.yaw);
plane.compass.setHIL(1, packet.roll, packet.pitch, packet.yaw);
// cope with DCM getting badly off due to HIL lag
if (plane.g.hil_err_limit > 0 &&
(fabsf(packet.roll - plane.ahrs.roll) > ToRad(plane.g.hil_err_limit) ||
fabsf(packet.pitch - plane.ahrs.pitch) > ToRad(plane.g.hil_err_limit) ||
wrap_PI(fabsf(packet.yaw - plane.ahrs.yaw)) > ToRad(plane.g.hil_err_limit))) {
plane.ahrs.reset_attitude(packet.roll, packet.pitch, packet.yaw);
}
#endif
break;
}
case MAVLINK_MSG_ID_RADIO:
case MAVLINK_MSG_ID_RADIO_STATUS:
{
handle_radio_status(msg, plane.should_log(MASK_LOG_PM));
break;
}
case MAVLINK_MSG_ID_DISTANCE_SENSOR:
plane.rangefinder.handle_msg(msg);
break;
case MAVLINK_MSG_ID_TERRAIN_DATA:
case MAVLINK_MSG_ID_TERRAIN_CHECK:
#if AP_TERRAIN_AVAILABLE
plane.terrain.handle_data(chan, msg);
#endif
break;
case MAVLINK_MSG_ID_SET_ATTITUDE_TARGET:
{
// Only allow companion computer (or other external controller) to
// control attitude in GUIDED mode. We DON'T want external control
// in e.g., RTL, CICLE. Specifying a single mode for companion
// computer control is more safe (even more so when using
// FENCE_ACTION = 4 for geofence failures).
if ((plane.control_mode != &plane.mode_guided) &&
(plane.control_mode != &plane.mode_avoidADSB)) { // don't screw up failsafes
break;
}
mavlink_set_attitude_target_t att_target;
mavlink_msg_set_attitude_target_decode(msg, &att_target);
// Mappings: If any of these bits are set, the corresponding input should be ignored.
// NOTE, when parsing the bits we invert them for easier interpretation but transport has them inverted
// bit 1: body roll rate
// bit 2: body pitch rate
// bit 3: body yaw rate
// bit 4: unknown
// bit 5: unknown
// bit 6: reserved
// bit 7: throttle
// bit 8: attitude
// if not setting all Quaternion values, use _rate flags to indicate which fields.
// Extract the Euler roll angle from the Quaternion.
Quaternion q(att_target.q[0], att_target.q[1],
att_target.q[2], att_target.q[3]);
// NOTE: att_target.type_mask is inverted for easier interpretation
att_target.type_mask = att_target.type_mask ^ 0xFF;
uint8_t attitude_mask = att_target.type_mask & 0b10000111; // q plus rpy
uint32_t now = AP_HAL::millis();
if ((attitude_mask & 0b10000001) || // partial, including roll
(attitude_mask == 0b10000000)) { // all angles
plane.guided_state.forced_rpy_cd.x = degrees(q.get_euler_roll()) * 100.0f;
// Update timer for external roll to the nav control
plane.guided_state.last_forced_rpy_ms.x = now;
}
if ((attitude_mask & 0b10000010) || // partial, including pitch
(attitude_mask == 0b10000000)) { // all angles
plane.guided_state.forced_rpy_cd.y = degrees(q.get_euler_pitch()) * 100.0f;
// Update timer for external pitch to the nav control
plane.guided_state.last_forced_rpy_ms.y = now;
}
if ((attitude_mask & 0b10000100) || // partial, including yaw
(attitude_mask == 0b10000000)) { // all angles
plane.guided_state.forced_rpy_cd.z = degrees(q.get_euler_yaw()) * 100.0f;
// Update timer for external yaw to the nav control
plane.guided_state.last_forced_rpy_ms.z = now;
}
if (att_target.type_mask & 0b01000000) { // throttle
plane.guided_state.forced_throttle = att_target.thrust * 100.0f;
// Update timer for external throttle
plane.guided_state.last_forced_throttle_ms = now;
}
break;
}
case MAVLINK_MSG_ID_SET_HOME_POSITION:
{
mavlink_set_home_position_t packet;
mavlink_msg_set_home_position_decode(msg, &packet);
Location new_home_loc {};
new_home_loc.lat = packet.latitude;
new_home_loc.lng = packet.longitude;
new_home_loc.alt = packet.altitude / 10;
if (!set_home(new_home_loc, false)) {
// silently fails...
break;
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED:
{
// decode packet
mavlink_set_position_target_local_ned_t packet;
mavlink_msg_set_position_target_local_ned_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (plane.control_mode != &plane.mode_guided) {
break;
}
// only local moves for now
if (packet.coordinate_frame != MAV_FRAME_LOCAL_OFFSET_NED) {
break;
}
// just do altitude for now
plane.next_WP_loc.alt += -packet.z*100.0;
gcs().send_text(MAV_SEVERITY_INFO, "Change alt to %.1f",
(double)((plane.next_WP_loc.alt - plane.home.alt)*0.01));
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT:
{
// Only want to allow companion computer position control when
// in a certain mode to avoid inadvertently sending these
// kinds of commands when the autopilot is responding to problems
// in modes such as RTL, CIRCLE, etc. Specifying ONLY one mode
// for companion computer control is more safe (provided
// one uses the FENCE_ACTION = 4 (RTL) for geofence failures).
if (plane.control_mode != &plane.mode_guided && plane.control_mode != &plane.mode_avoidADSB) {
//don't screw up failsafes
break;
}
mavlink_set_position_target_global_int_t pos_target;
mavlink_msg_set_position_target_global_int_decode(msg, &pos_target);
// Unexpectedly, the mask is expecting "ones" for dimensions that should
// be IGNORNED rather than INCLUDED. See mavlink documentation of the
// SET_POSITION_TARGET_GLOBAL_INT message, type_mask field.
const uint16_t alt_mask = 0b1111111111111011; // (z mask at bit 3)
bool msg_valid = true;
AP_Mission::Mission_Command cmd = {0};
if (pos_target.type_mask & alt_mask)
{
cmd.content.location.alt = pos_target.alt * 100;
cmd.content.location.relative_alt = false;
cmd.content.location.terrain_alt = false;
switch (pos_target.coordinate_frame)
{
case MAV_FRAME_GLOBAL_INT:
break; //default to MSL altitude
case MAV_FRAME_GLOBAL_RELATIVE_ALT_INT:
cmd.content.location.relative_alt = true;
break;
case MAV_FRAME_GLOBAL_TERRAIN_ALT_INT:
cmd.content.location.relative_alt = true;
cmd.content.location.terrain_alt = true;
break;
default:
gcs().send_text(MAV_SEVERITY_WARNING, "Invalid coord frame in SET_POSTION_TARGET_GLOBAL_INT");
msg_valid = false;
break;
}
if (msg_valid) {
handle_change_alt_request(cmd);
}
} // end if alt_mask
break;
}
case MAVLINK_MSG_ID_ADSB_VEHICLE:
case MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_CFG:
case MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC:
case MAVLINK_MSG_ID_UAVIONIX_ADSB_TRANSCEIVER_HEALTH_REPORT:
plane.adsb.handle_message(chan, msg);
break;
default:
handle_common_message(msg);
break;
} // end switch
} // end handle mavlink
static void
handle_message(mavlink_message_t *msg)
{
if (msg->msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
mavlink_command_long_t cmd_mavlink;
mavlink_msg_command_long_decode(msg, &cmd_mavlink);
if (cmd_mavlink.target_system == mavlink_system.sysid && ((cmd_mavlink.target_component == mavlink_system.compid)
|| (cmd_mavlink.target_component == MAV_COMP_ID_ALL))) {
//check for MAVLINK terminate command
if (cmd_mavlink.command == MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN && ((int)cmd_mavlink.param1) == 3) {
/* This is the link shutdown command, terminate mavlink */
printf("[mavlink] Terminating .. \n");
fflush(stdout);
usleep(50000);
/* terminate other threads and this thread */
thread_should_exit = true;
} else {
/* Copy the content of mavlink_command_long_t cmd_mavlink into command_t cmd */
vcmd.param1 = cmd_mavlink.param1;
vcmd.param2 = cmd_mavlink.param2;
vcmd.param3 = cmd_mavlink.param3;
vcmd.param4 = cmd_mavlink.param4;
vcmd.param5 = cmd_mavlink.param5;
vcmd.param6 = cmd_mavlink.param6;
vcmd.param7 = cmd_mavlink.param7;
// XXX do proper translation
vcmd.command = (enum VEHICLE_CMD)cmd_mavlink.command;
vcmd.target_system = cmd_mavlink.target_system;
vcmd.target_component = cmd_mavlink.target_component;
vcmd.source_system = msg->sysid;
vcmd.source_component = msg->compid;
vcmd.confirmation = cmd_mavlink.confirmation;
/* check if topic is advertised */
if (cmd_pub <= 0) {
cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd);
} else {
/* publish */
orb_publish(ORB_ID(vehicle_command), cmd_pub, &vcmd);
}
}
}
}
if (msg->msgid == MAVLINK_MSG_ID_OPTICAL_FLOW) {
mavlink_optical_flow_t flow;
mavlink_msg_optical_flow_decode(msg, &flow);
struct optical_flow_s f;
f.timestamp = flow.time_usec;
f.flow_raw_x = flow.flow_x;
f.flow_raw_y = flow.flow_y;
f.flow_comp_x_m = flow.flow_comp_m_x;
f.flow_comp_y_m = flow.flow_comp_m_y;
f.ground_distance_m = flow.ground_distance;
f.quality = flow.quality;
f.sensor_id = flow.sensor_id;
/* check if topic is advertised */
if (flow_pub <= 0) {
flow_pub = orb_advertise(ORB_ID(optical_flow), &f);
} else {
/* publish */
orb_publish(ORB_ID(optical_flow), flow_pub, &f);
}
}
if (msg->msgid == MAVLINK_MSG_ID_SET_MODE) {
/* Set mode on request */
mavlink_set_mode_t new_mode;
mavlink_msg_set_mode_decode(msg, &new_mode);
union px4_custom_mode custom_mode;
custom_mode.data = new_mode.custom_mode;
/* Copy the content of mavlink_command_long_t cmd_mavlink into command_t cmd */
vcmd.param1 = new_mode.base_mode;
vcmd.param2 = custom_mode.main_mode;
vcmd.param3 = 0;
vcmd.param4 = 0;
vcmd.param5 = 0;
vcmd.param6 = 0;
vcmd.param7 = 0;
vcmd.command = VEHICLE_CMD_DO_SET_MODE;
vcmd.target_system = new_mode.target_system;
vcmd.target_component = MAV_COMP_ID_ALL;
vcmd.source_system = msg->sysid;
vcmd.source_component = msg->compid;
vcmd.confirmation = 1;
/* check if topic is advertised */
if (cmd_pub <= 0) {
cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd);
} else {
/* create command */
orb_publish(ORB_ID(vehicle_command), cmd_pub, &vcmd);
}
}
/* Handle Vicon position estimates */
if (msg->msgid == MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE) {
mavlink_vicon_position_estimate_t pos;
mavlink_msg_vicon_position_estimate_decode(msg, &pos);
vicon_position.timestamp = hrt_absolute_time();
vicon_position.x = pos.x;
vicon_position.y = pos.y;
vicon_position.z = pos.z;
vicon_position.roll = pos.roll;
vicon_position.pitch = pos.pitch;
vicon_position.yaw = pos.yaw;
if (vicon_position_pub <= 0) {
vicon_position_pub = orb_advertise(ORB_ID(vehicle_vicon_position), &vicon_position);
} else {
orb_publish(ORB_ID(vehicle_vicon_position), vicon_position_pub, &vicon_position);
}
}
/* Handle quadrotor motor setpoints */
if (msg->msgid == MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST) {
mavlink_set_quad_swarm_roll_pitch_yaw_thrust_t quad_motors_setpoint;
mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust_decode(msg, &quad_motors_setpoint);
if (mavlink_system.sysid < 4) {
/* switch to a receiving link mode */
gcs_link = false;
/*
* rate control mode - defined by MAVLink
*/
uint8_t ml_mode = 0;
bool ml_armed = false;
switch (quad_motors_setpoint.mode) {
case 0:
ml_armed = false;
break;
case 1:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_RATES;
ml_armed = true;
break;
case 2:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE;
ml_armed = true;
break;
case 3:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_VELOCITY;
break;
case 4:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_POSITION;
break;
}
offboard_control_sp.p1 = (float)quad_motors_setpoint.roll[mavlink_system.sysid - 1] / (float)INT16_MAX;
offboard_control_sp.p2 = (float)quad_motors_setpoint.pitch[mavlink_system.sysid - 1] / (float)INT16_MAX;
offboard_control_sp.p3 = (float)quad_motors_setpoint.yaw[mavlink_system.sysid - 1] / (float)INT16_MAX;
offboard_control_sp.p4 = (float)quad_motors_setpoint.thrust[mavlink_system.sysid - 1] / (float)UINT16_MAX;
if (quad_motors_setpoint.thrust[mavlink_system.sysid - 1] == 0) {
ml_armed = false;
}
offboard_control_sp.armed = ml_armed;
offboard_control_sp.mode = static_cast<enum OFFBOARD_CONTROL_MODE>(ml_mode);
offboard_control_sp.timestamp = hrt_absolute_time();
/* check if topic has to be advertised */
if (offboard_control_sp_pub <= 0) {
offboard_control_sp_pub = orb_advertise(ORB_ID(offboard_control_setpoint), &offboard_control_sp);
} else {
/* Publish */
orb_publish(ORB_ID(offboard_control_setpoint), offboard_control_sp_pub, &offboard_control_sp);
}
}
}
/* handle status updates of the radio */
if (msg->msgid == MAVLINK_MSG_ID_RADIO_STATUS) {
struct telemetry_status_s tstatus;
mavlink_radio_status_t rstatus;
mavlink_msg_radio_status_decode(msg, &rstatus);
/* publish telemetry status topic */
tstatus.timestamp = hrt_absolute_time();
tstatus.type = TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO;
tstatus.rssi = rstatus.rssi;
tstatus.remote_rssi = rstatus.remrssi;
tstatus.txbuf = rstatus.txbuf;
tstatus.noise = rstatus.noise;
tstatus.remote_noise = rstatus.remnoise;
tstatus.rxerrors = rstatus.rxerrors;
tstatus.fixed = rstatus.fixed;
if (telemetry_status_pub == 0) {
telemetry_status_pub = orb_advertise(ORB_ID(telemetry_status), &tstatus);
} else {
orb_publish(ORB_ID(telemetry_status), telemetry_status_pub, &tstatus);
}
}
/*
* Only decode hil messages in HIL mode.
*
* The HIL mode is enabled by the HIL bit flag
* in the system mode. Either send a set mode
* COMMAND_LONG message or a SET_MODE message
*/
if (mavlink_hil_enabled) {
uint64_t timestamp = hrt_absolute_time();
if (msg->msgid == MAVLINK_MSG_ID_HIL_SENSOR) {
mavlink_hil_sensor_t imu;
mavlink_msg_hil_sensor_decode(msg, &imu);
/* sensors general */
hil_sensors.timestamp = hrt_absolute_time();
/* hil gyro */
static const float mrad2rad = 1.0e-3f;
hil_sensors.gyro_counter = hil_counter;
hil_sensors.gyro_raw[0] = imu.xgyro / mrad2rad;
hil_sensors.gyro_raw[1] = imu.ygyro / mrad2rad;
hil_sensors.gyro_raw[2] = imu.zgyro / mrad2rad;
hil_sensors.gyro_rad_s[0] = imu.xgyro;
hil_sensors.gyro_rad_s[1] = imu.ygyro;
hil_sensors.gyro_rad_s[2] = imu.zgyro;
/* accelerometer */
hil_sensors.accelerometer_counter = hil_counter;
static const float mg2ms2 = 9.8f / 1000.0f;
hil_sensors.accelerometer_raw[0] = imu.xacc / mg2ms2;
hil_sensors.accelerometer_raw[1] = imu.yacc / mg2ms2;
hil_sensors.accelerometer_raw[2] = imu.zacc / mg2ms2;
hil_sensors.accelerometer_m_s2[0] = imu.xacc;
hil_sensors.accelerometer_m_s2[1] = imu.yacc;
hil_sensors.accelerometer_m_s2[2] = imu.zacc;
hil_sensors.accelerometer_mode = 0; // TODO what is this?
hil_sensors.accelerometer_range_m_s2 = 32.7f; // int16
/* adc */
hil_sensors.adc_voltage_v[0] = 0.0f;
hil_sensors.adc_voltage_v[1] = 0.0f;
hil_sensors.adc_voltage_v[2] = 0.0f;
/* magnetometer */
float mga2ga = 1.0e-3f;
hil_sensors.magnetometer_counter = hil_counter;
hil_sensors.magnetometer_raw[0] = imu.xmag / mga2ga;
hil_sensors.magnetometer_raw[1] = imu.ymag / mga2ga;
hil_sensors.magnetometer_raw[2] = imu.zmag / mga2ga;
hil_sensors.magnetometer_ga[0] = imu.xmag;
hil_sensors.magnetometer_ga[1] = imu.ymag;
hil_sensors.magnetometer_ga[2] = imu.zmag;
hil_sensors.magnetometer_range_ga = 32.7f; // int16
hil_sensors.magnetometer_mode = 0; // TODO what is this
hil_sensors.magnetometer_cuttoff_freq_hz = 50.0f;
/* baro */
hil_sensors.baro_pres_mbar = imu.abs_pressure;
hil_sensors.baro_alt_meter = imu.pressure_alt;
hil_sensors.baro_temp_celcius = imu.temperature;
hil_sensors.gyro_counter = hil_counter;
hil_sensors.magnetometer_counter = hil_counter;
hil_sensors.accelerometer_counter = hil_counter;
/* differential pressure */
hil_sensors.differential_pressure_pa = imu.diff_pressure * 1e2f; //from hPa to Pa
hil_sensors.differential_pressure_counter = hil_counter;
/* airspeed from differential pressure, ambient pressure and temp */
struct airspeed_s airspeed;
float ias = calc_indicated_airspeed(hil_sensors.differential_pressure_pa);
// XXX need to fix this
float tas = ias;
airspeed.timestamp = hrt_absolute_time();
airspeed.indicated_airspeed_m_s = ias;
airspeed.true_airspeed_m_s = tas;
if (pub_hil_airspeed < 0) {
pub_hil_airspeed = orb_advertise(ORB_ID(airspeed), &airspeed);
} else {
orb_publish(ORB_ID(airspeed), pub_hil_airspeed, &airspeed);
}
//warnx("SENSOR: IAS: %6.2f TAS: %6.2f", airspeed.indicated_airspeed_m_s, airspeed.true_airspeed_m_s);
/* individual sensor publications */
struct gyro_report gyro;
gyro.x_raw = imu.xgyro / mrad2rad;
gyro.y_raw = imu.ygyro / mrad2rad;
gyro.z_raw = imu.zgyro / mrad2rad;
gyro.x = imu.xgyro;
gyro.y = imu.ygyro;
gyro.z = imu.zgyro;
gyro.temperature = imu.temperature;
gyro.timestamp = hrt_absolute_time();
if (pub_hil_gyro < 0) {
pub_hil_gyro = orb_advertise(ORB_ID(sensor_gyro), &gyro);
} else {
orb_publish(ORB_ID(sensor_gyro), pub_hil_gyro, &gyro);
}
struct accel_report accel;
accel.x_raw = imu.xacc / mg2ms2;
accel.y_raw = imu.yacc / mg2ms2;
accel.z_raw = imu.zacc / mg2ms2;
accel.x = imu.xacc;
accel.y = imu.yacc;
accel.z = imu.zacc;
accel.temperature = imu.temperature;
accel.timestamp = hrt_absolute_time();
if (pub_hil_accel < 0) {
pub_hil_accel = orb_advertise(ORB_ID(sensor_accel), &accel);
} else {
orb_publish(ORB_ID(sensor_accel), pub_hil_accel, &accel);
}
struct mag_report mag;
mag.x_raw = imu.xmag / mga2ga;
mag.y_raw = imu.ymag / mga2ga;
mag.z_raw = imu.zmag / mga2ga;
mag.x = imu.xmag;
mag.y = imu.ymag;
mag.z = imu.zmag;
mag.timestamp = hrt_absolute_time();
if (pub_hil_mag < 0) {
pub_hil_mag = orb_advertise(ORB_ID(sensor_mag), &mag);
} else {
orb_publish(ORB_ID(sensor_mag), pub_hil_mag, &mag);
}
struct baro_report baro;
baro.pressure = imu.abs_pressure;
baro.altitude = imu.pressure_alt;
baro.temperature = imu.temperature;
baro.timestamp = hrt_absolute_time();
if (pub_hil_baro < 0) {
pub_hil_baro = orb_advertise(ORB_ID(sensor_baro), &baro);
} else {
orb_publish(ORB_ID(sensor_baro), pub_hil_baro, &baro);
}
/* publish combined sensor topic */
if (pub_hil_sensors > 0) {
orb_publish(ORB_ID(sensor_combined), pub_hil_sensors, &hil_sensors);
} else {
pub_hil_sensors = orb_advertise(ORB_ID(sensor_combined), &hil_sensors);
}
/* fill in HIL battery status */
hil_battery_status.timestamp = hrt_absolute_time();
hil_battery_status.voltage_v = 11.1f;
hil_battery_status.current_a = 10.0f;
/* lazily publish the battery voltage */
if (pub_hil_battery > 0) {
orb_publish(ORB_ID(battery_status), pub_hil_battery, &hil_battery_status);
} else {
pub_hil_battery = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
}
// increment counters
hil_counter++;
hil_frames++;
// output
if ((timestamp - old_timestamp) > 10000000) {
printf("receiving hil sensor at %d hz\n", hil_frames / 10);
old_timestamp = timestamp;
hil_frames = 0;
}
}
if (msg->msgid == MAVLINK_MSG_ID_HIL_GPS) {
mavlink_hil_gps_t gps;
mavlink_msg_hil_gps_decode(msg, &gps);
/* gps */
hil_gps.timestamp_position = gps.time_usec;
hil_gps.time_gps_usec = gps.time_usec;
hil_gps.lat = gps.lat;
hil_gps.lon = gps.lon;
hil_gps.alt = gps.alt;
hil_gps.eph_m = (float)gps.eph * 1e-2f; // from cm to m
hil_gps.epv_m = (float)gps.epv * 1e-2f; // from cm to m
hil_gps.s_variance_m_s = 5.0f;
hil_gps.p_variance_m = hil_gps.eph_m * hil_gps.eph_m;
hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
/* gps.cog is in degrees 0..360 * 100, heading is -PI..+PI */
float heading_rad = gps.cog * M_DEG_TO_RAD_F * 1e-2f;
/* go back to -PI..PI */
if (heading_rad > M_PI_F)
heading_rad -= 2.0f * M_PI_F;
hil_gps.vel_n_m_s = gps.vn * 1e-2f; // from cm to m
hil_gps.vel_e_m_s = gps.ve * 1e-2f; // from cm to m
hil_gps.vel_d_m_s = gps.vd * 1e-2f; // from cm to m
hil_gps.vel_ned_valid = true;
/* COG (course over ground) is spec'ed as -PI..+PI */
hil_gps.cog_rad = heading_rad;
hil_gps.fix_type = gps.fix_type;
hil_gps.satellites_visible = gps.satellites_visible;
/* publish GPS measurement data */
if (pub_hil_gps > 0) {
orb_publish(ORB_ID(vehicle_gps_position), pub_hil_gps, &hil_gps);
} else {
pub_hil_gps = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps);
}
}
if (msg->msgid == MAVLINK_MSG_ID_HIL_STATE_QUATERNION) {
mavlink_hil_state_quaternion_t hil_state;
mavlink_msg_hil_state_quaternion_decode(msg, &hil_state);
struct airspeed_s airspeed;
airspeed.timestamp = hrt_absolute_time();
airspeed.indicated_airspeed_m_s = hil_state.ind_airspeed * 1e-2f;
airspeed.true_airspeed_m_s = hil_state.true_airspeed * 1e-2f;
if (pub_hil_airspeed < 0) {
pub_hil_airspeed = orb_advertise(ORB_ID(airspeed), &airspeed);
} else {
orb_publish(ORB_ID(airspeed), pub_hil_airspeed, &airspeed);
}
uint64_t timestamp = hrt_absolute_time();
// publish global position
if (pub_hil_global_pos > 0) {
orb_publish(ORB_ID(vehicle_global_position), pub_hil_global_pos, &hil_global_pos);
// global position packet
hil_global_pos.timestamp = timestamp;
hil_global_pos.valid = true;
hil_global_pos.lat = hil_state.lat;
hil_global_pos.lon = hil_state.lon;
hil_global_pos.alt = hil_state.alt / 1000.0f;
hil_global_pos.vx = hil_state.vx / 100.0f;
hil_global_pos.vy = hil_state.vy / 100.0f;
hil_global_pos.vz = hil_state.vz / 100.0f;
} else {
pub_hil_global_pos = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos);
}
// publish local position
if (pub_hil_local_pos > 0) {
float x;
float y;
bool landed = hil_state.alt/1000.0f < (alt0 + 0.1); // XXX improve?
double lat = hil_state.lat*1e-7;
double lon = hil_state.lon*1e-7;
map_projection_project(lat, lon, &x, &y);
hil_local_pos.timestamp = timestamp;
hil_local_pos.xy_valid = true;
hil_local_pos.z_valid = true;
hil_local_pos.v_xy_valid = true;
hil_local_pos.v_z_valid = true;
hil_local_pos.x = x;
hil_local_pos.y = y;
hil_local_pos.z = alt0 - hil_state.alt/1000.0f;
hil_local_pos.vx = hil_state.vx/100.0f;
hil_local_pos.vy = hil_state.vy/100.0f;
hil_local_pos.vz = hil_state.vz/100.0f;
hil_local_pos.yaw = hil_attitude.yaw;
hil_local_pos.xy_global = true;
hil_local_pos.z_global = true;
hil_local_pos.ref_timestamp = timestamp;
hil_local_pos.ref_lat = hil_state.lat;
hil_local_pos.ref_lon = hil_state.lon;
hil_local_pos.ref_alt = alt0;
hil_local_pos.landed = landed;
orb_publish(ORB_ID(vehicle_local_position), pub_hil_local_pos, &hil_local_pos);
} else {
pub_hil_local_pos = orb_advertise(ORB_ID(vehicle_local_position), &hil_local_pos);
lat0 = hil_state.lat;
lon0 = hil_state.lon;
alt0 = hil_state.alt / 1000.0f;
map_projection_init(hil_state.lat, hil_state.lon);
}
/* Calculate Rotation Matrix */
math::Quaternion q(hil_state.attitude_quaternion);
math::Dcm C_nb(q);
math::EulerAngles euler(C_nb);
/* set rotation matrix */
for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++)
hil_attitude.R[i][j] = C_nb(i, j);
hil_attitude.R_valid = true;
/* set quaternion */
hil_attitude.q[0] = q(0);
hil_attitude.q[1] = q(1);
hil_attitude.q[2] = q(2);
hil_attitude.q[3] = q(3);
hil_attitude.q_valid = true;
hil_attitude.roll = euler.getPhi();
hil_attitude.pitch = euler.getTheta();
hil_attitude.yaw = euler.getPsi();
hil_attitude.rollspeed = hil_state.rollspeed;
hil_attitude.pitchspeed = hil_state.pitchspeed;
hil_attitude.yawspeed = hil_state.yawspeed;
/* set timestamp and notify processes (broadcast) */
hil_attitude.timestamp = hrt_absolute_time();
if (pub_hil_attitude > 0) {
orb_publish(ORB_ID(vehicle_attitude), pub_hil_attitude, &hil_attitude);
} else {
pub_hil_attitude = orb_advertise(ORB_ID(vehicle_attitude), &hil_attitude);
}
struct accel_report accel;
accel.x_raw = hil_state.xacc / 9.81f * 1e3f;
accel.y_raw = hil_state.yacc / 9.81f * 1e3f;
accel.z_raw = hil_state.zacc / 9.81f * 1e3f;
accel.x = hil_state.xacc;
accel.y = hil_state.yacc;
accel.z = hil_state.zacc;
accel.temperature = 25.0f;
accel.timestamp = hrt_absolute_time();
if (pub_hil_accel < 0) {
pub_hil_accel = orb_advertise(ORB_ID(sensor_accel), &accel);
} else {
orb_publish(ORB_ID(sensor_accel), pub_hil_accel, &accel);
}
/* fill in HIL battery status */
hil_battery_status.timestamp = hrt_absolute_time();
hil_battery_status.voltage_v = 11.1f;
hil_battery_status.current_a = 10.0f;
/* lazily publish the battery voltage */
if (pub_hil_battery > 0) {
orb_publish(ORB_ID(battery_status), pub_hil_battery, &hil_battery_status);
} else {
pub_hil_battery = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
}
}
if (msg->msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) {
mavlink_manual_control_t man;
mavlink_msg_manual_control_decode(msg, &man);
struct rc_channels_s rc_hil;
memset(&rc_hil, 0, sizeof(rc_hil));
static orb_advert_t rc_pub = 0;
rc_hil.timestamp = hrt_absolute_time();
rc_hil.chan_count = 4;
rc_hil.chan[0].scaled = man.x / 1000.0f;
rc_hil.chan[1].scaled = man.y / 1000.0f;
rc_hil.chan[2].scaled = man.r / 1000.0f;
rc_hil.chan[3].scaled = man.z / 1000.0f;
struct manual_control_setpoint_s mc;
static orb_advert_t mc_pub = 0;
int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
/* get a copy first, to prevent altering values that are not sent by the mavlink command */
orb_copy(ORB_ID(manual_control_setpoint), manual_sub, &mc);
mc.timestamp = rc_hil.timestamp;
mc.roll = man.x / 1000.0f;
mc.pitch = man.y / 1000.0f;
mc.yaw = man.r / 1000.0f;
mc.throttle = man.z / 1000.0f;
/* fake RC channels with manual control input from simulator */
if (rc_pub == 0) {
rc_pub = orb_advertise(ORB_ID(rc_channels), &rc_hil);
} else {
orb_publish(ORB_ID(rc_channels), rc_pub, &rc_hil);
}
if (mc_pub == 0) {
mc_pub = orb_advertise(ORB_ID(manual_control_setpoint), &mc);
} else {
orb_publish(ORB_ID(manual_control_setpoint), mc_pub, &mc);
}
}
}
}
void GCS_MAVLINK_Rover::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
case MAVLINK_MSG_ID_REQUEST_DATA_STREAM:
{
handle_request_data_stream(msg, true);
break;
}
case MAVLINK_MSG_ID_COMMAND_INT: {
// decode packet
mavlink_command_int_t packet;
mavlink_msg_command_int_decode(msg, &packet);
MAV_RESULT result = MAV_RESULT_UNSUPPORTED;
switch (packet.command) {
case MAV_CMD_DO_SET_HOME: {
// assume failure
result = MAV_RESULT_FAILED;
if (is_equal(packet.param1, 1.0f)) {
// if param1 is 1, use current location
if (rover.set_home_to_current_location(true)) {
result = MAV_RESULT_ACCEPTED;
}
break;
}
// ensure param1 is zero
if (!is_zero(packet.param1)) {
break;
}
// check frame type is supported
if (packet.frame != MAV_FRAME_GLOBAL &&
packet.frame != MAV_FRAME_GLOBAL_INT &&
packet.frame != MAV_FRAME_GLOBAL_RELATIVE_ALT &&
packet.frame != MAV_FRAME_GLOBAL_RELATIVE_ALT_INT) {
break;
}
// sanity check location
if (!check_latlng(packet.x, packet.y)) {
break;
}
Location new_home_loc {};
new_home_loc.lat = packet.x;
new_home_loc.lng = packet.y;
new_home_loc.alt = packet.z * 100;
// handle relative altitude
if (packet.frame == MAV_FRAME_GLOBAL_RELATIVE_ALT || packet.frame == MAV_FRAME_GLOBAL_RELATIVE_ALT_INT) {
if (!rover.ahrs.home_is_set()) {
// cannot use relative altitude if home is not set
break;
}
new_home_loc.alt += rover.ahrs.get_home().alt;
}
if (rover.set_home(new_home_loc, true)) {
result = MAV_RESULT_ACCEPTED;
}
break;
}
#if MOUNT == ENABLED
case MAV_CMD_DO_SET_ROI: {
// param1 : /* Region of interest mode (not used)*/
// param2 : /* MISSION index/ target ID (not used)*/
// param3 : /* ROI index (not used)*/
// param4 : /* empty */
// x : lat
// y : lon
// z : alt
// sanity check location
if (!check_latlng(packet.x, packet.y)) {
break;
}
Location roi_loc;
roi_loc.lat = packet.x;
roi_loc.lng = packet.y;
roi_loc.alt = (int32_t)(packet.z * 100.0f);
if (roi_loc.lat == 0 && roi_loc.lng == 0 && roi_loc.alt == 0) {
// switch off the camera tracking if enabled
if (rover.camera_mount.get_mode() == MAV_MOUNT_MODE_GPS_POINT) {
rover.camera_mount.set_mode_to_default();
}
} else {
// send the command to the camera mount
rover.camera_mount.set_roi_target(roi_loc);
}
result = MAV_RESULT_ACCEPTED;
break;
}
#endif
default:
result = MAV_RESULT_UNSUPPORTED;
break;
}
// send ACK or NAK
mavlink_msg_command_ack_send_buf(msg, chan, packet.command, result);
break;
}
case MAVLINK_MSG_ID_COMMAND_LONG:
{
// decode
mavlink_command_long_t packet;
mavlink_msg_command_long_decode(msg, &packet);
MAV_RESULT result = MAV_RESULT_UNSUPPORTED;
// do command
switch (packet.command) {
case MAV_CMD_NAV_RETURN_TO_LAUNCH:
rover.set_mode(rover.mode_rtl, MODE_REASON_GCS_COMMAND);
result = MAV_RESULT_ACCEPTED;
break;
#if MOUNT == ENABLED
// Sets the region of interest (ROI) for the camera
case MAV_CMD_DO_SET_ROI:
// sanity check location
if (!check_latlng(packet.param5, packet.param6)) {
break;
}
Location roi_loc;
roi_loc.lat = (int32_t)(packet.param5 * 1.0e7f);
roi_loc.lng = (int32_t)(packet.param6 * 1.0e7f);
roi_loc.alt = (int32_t)(packet.param7 * 100.0f);
if (roi_loc.lat == 0 && roi_loc.lng == 0 && roi_loc.alt == 0) {
// switch off the camera tracking if enabled
if (rover.camera_mount.get_mode() == MAV_MOUNT_MODE_GPS_POINT) {
rover.camera_mount.set_mode_to_default();
}
} else {
// send the command to the camera mount
rover.camera_mount.set_roi_target(roi_loc);
}
result = MAV_RESULT_ACCEPTED;
break;
#endif
case MAV_CMD_DO_MOUNT_CONTROL:
#if MOUNT == ENABLED
rover.camera_mount.control(packet.param1, packet.param2, packet.param3, (MAV_MOUNT_MODE) packet.param7);
result = MAV_RESULT_ACCEPTED;
#endif
break;
case MAV_CMD_MISSION_START:
rover.set_mode(rover.mode_auto, MODE_REASON_GCS_COMMAND);
result = MAV_RESULT_ACCEPTED;
break;
case MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN:
if (is_equal(packet.param1, 1.0f) || is_equal(packet.param1, 3.0f)) {
// when packet.param1 == 3 we reboot to hold in bootloader
hal.scheduler->reboot(is_equal(packet.param1, 3.0f));
result = MAV_RESULT_ACCEPTED;
}
break;
case MAV_CMD_COMPONENT_ARM_DISARM:
if (is_equal(packet.param1, 1.0f)) {
// run pre_arm_checks and arm_checks and display failures
if (rover.arm_motors(AP_Arming::MAVLINK)) {
result = MAV_RESULT_ACCEPTED;
} else {
result = MAV_RESULT_FAILED;
}
} else if (is_zero(packet.param1)) {
if (rover.disarm_motors()) {
result = MAV_RESULT_ACCEPTED;
} else {
result = MAV_RESULT_FAILED;
}
} else {
result = MAV_RESULT_UNSUPPORTED;
}
break;
case MAV_CMD_DO_FENCE_ENABLE:
result = MAV_RESULT_ACCEPTED;
switch ((uint16_t)packet.param1) {
case 0:
rover.g2.fence.enable(false);
break;
case 1:
rover.g2.fence.enable(true);
break;
default:
result = MAV_RESULT_FAILED;
break;
}
break;
case MAV_CMD_DO_SET_HOME:
{
// param1 : use current (1=use current location, 0=use specified location)
// param5 : latitude
// param6 : longitude
// param7 : altitude
result = MAV_RESULT_FAILED; // assume failure
if (is_equal(packet.param1, 1.0f)) {
if (rover.set_home_to_current_location(true)) {
result = MAV_RESULT_ACCEPTED;
}
} else {
// ensure param1 is zero
if (!is_zero(packet.param1)) {
break;
}
Location new_home_loc {};
new_home_loc.lat = static_cast<int32_t>(packet.param5 * 1.0e7f);
new_home_loc.lng = static_cast<int32_t>(packet.param6 * 1.0e7f);
new_home_loc.alt = static_cast<int32_t>(packet.param7 * 100.0f);
if (rover.set_home(new_home_loc, true)) {
result = MAV_RESULT_ACCEPTED;
}
}
break;
}
case MAV_CMD_NAV_SET_YAW_SPEED:
{
// param1 : yaw angle to adjust direction by in centidegress
// param2 : Speed - normalized to 0 .. 1
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// send yaw change and target speed to guided mode controller
const float speed_max = rover.control_mode->get_speed_default();
const float target_speed = constrain_float(packet.param2 * speed_max, -speed_max, speed_max);
rover.mode_guided.set_desired_heading_delta_and_speed(packet.param1, target_speed);
result = MAV_RESULT_ACCEPTED;
break;
}
case MAV_CMD_ACCELCAL_VEHICLE_POS:
result = MAV_RESULT_FAILED;
if (rover.ins.get_acal()->gcs_vehicle_position(packet.param1)) {
result = MAV_RESULT_ACCEPTED;
}
break;
case MAV_CMD_DO_MOTOR_TEST:
// param1 : motor sequence number (a number from 1 to max number of motors on the vehicle)
// param2 : throttle type (0=throttle percentage, 1=PWM, 2=pilot throttle channel pass-through. See MOTOR_TEST_THROTTLE_TYPE enum)
// param3 : throttle (range depends upon param2)
// param4 : timeout (in seconds)
result = rover.mavlink_motor_test_start(chan, static_cast<uint8_t>(packet.param1),
static_cast<uint8_t>(packet.param2),
static_cast<int16_t>(packet.param3),
packet.param4);
break;
default:
result = handle_command_long_message(packet);
break;
}
mavlink_msg_command_ack_send_buf(
msg,
chan,
packet.command,
result);
break;
}
case MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE:
{
// allow override of RC channel values for HIL
// or for complete GCS control of switch position
// and RC PWM values.
if (msg->sysid != rover.g.sysid_my_gcs) { // Only accept control from our gcs
break;
}
mavlink_rc_channels_override_t packet;
mavlink_msg_rc_channels_override_decode(msg, &packet);
RC_Channels::set_override(0, packet.chan1_raw);
RC_Channels::set_override(1, packet.chan2_raw);
RC_Channels::set_override(2, packet.chan3_raw);
RC_Channels::set_override(3, packet.chan4_raw);
RC_Channels::set_override(4, packet.chan5_raw);
RC_Channels::set_override(5, packet.chan6_raw);
RC_Channels::set_override(6, packet.chan7_raw);
RC_Channels::set_override(7, packet.chan8_raw);
rover.failsafe.rc_override_timer = AP_HAL::millis();
rover.failsafe_trigger(FAILSAFE_EVENT_RC, false);
break;
}
case MAVLINK_MSG_ID_MANUAL_CONTROL:
{
if (msg->sysid != rover.g.sysid_my_gcs) { // Only accept control from our gcs
break;
}
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
if (packet.target != rover.g.sysid_this_mav) {
break; // only accept control aimed at us
}
const int16_t roll = (packet.y == INT16_MAX) ? 0 : rover.channel_steer->get_radio_min() + (rover.channel_steer->get_radio_max() - rover.channel_steer->get_radio_min()) * (packet.y + 1000) / 2000.0f;
const int16_t throttle = (packet.z == INT16_MAX) ? 0 : rover.channel_throttle->get_radio_min() + (rover.channel_throttle->get_radio_max() - rover.channel_throttle->get_radio_min()) * (packet.z + 1000) / 2000.0f;
RC_Channels::set_override(uint8_t(rover.rcmap.roll() - 1), roll);
RC_Channels::set_override(uint8_t(rover.rcmap.throttle() - 1), throttle);
rover.failsafe.rc_override_timer = AP_HAL::millis();
rover.failsafe_trigger(FAILSAFE_EVENT_RC, false);
break;
}
case MAVLINK_MSG_ID_HEARTBEAT:
{
// We keep track of the last time we received a heartbeat from our GCS for failsafe purposes
if (msg->sysid != rover.g.sysid_my_gcs) {
break;
}
rover.last_heartbeat_ms = rover.failsafe.rc_override_timer = AP_HAL::millis();
rover.failsafe_trigger(FAILSAFE_EVENT_GCS, false);
break;
}
case MAVLINK_MSG_ID_SET_ATTITUDE_TARGET: // MAV ID: 82
{
// decode packet
mavlink_set_attitude_target_t packet;
mavlink_msg_set_attitude_target_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// ensure type_mask specifies to use thrust
if ((packet.type_mask & MAVLINK_SET_ATT_TYPE_MASK_THROTTLE_IGNORE) != 0) {
break;
}
// convert thrust to ground speed
packet.thrust = constrain_float(packet.thrust, -1.0f, 1.0f);
const float target_speed = rover.control_mode->get_speed_default() * packet.thrust;
// if the body_yaw_rate field is ignored, convert quaternion to heading
if ((packet.type_mask & MAVLINK_SET_ATT_TYPE_MASK_YAW_RATE_IGNORE) != 0) {
// convert quaternion to heading
float target_heading_cd = degrees(Quaternion(packet.q[0], packet.q[1], packet.q[2], packet.q[3]).get_euler_yaw()) * 100.0f;
rover.mode_guided.set_desired_heading_and_speed(target_heading_cd, target_speed);
} else {
// use body_yaw_rate field
rover.mode_guided.set_desired_turn_rate_and_speed((RAD_TO_DEG * packet.body_yaw_rate) * 100.0f, target_speed);
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED: // MAV ID: 84
{
// decode packet
mavlink_set_position_target_local_ned_t packet;
mavlink_msg_set_position_target_local_ned_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_LOCAL_NED &&
packet.coordinate_frame != MAV_FRAME_LOCAL_OFFSET_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_OFFSET_NED) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
// prepare target position
Location target_loc = rover.current_loc;
if (!pos_ignore) {
switch (packet.coordinate_frame) {
case MAV_FRAME_BODY_NED:
case MAV_FRAME_BODY_OFFSET_NED: {
// rotate from body-frame to NE frame
const float ne_x = packet.x * rover.ahrs.cos_yaw() - packet.y * rover.ahrs.sin_yaw();
const float ne_y = packet.x * rover.ahrs.sin_yaw() + packet.y * rover.ahrs.cos_yaw();
// add offset to current location
location_offset(target_loc, ne_x, ne_y);
}
break;
case MAV_FRAME_LOCAL_OFFSET_NED:
// add offset to current location
location_offset(target_loc, packet.x, packet.y);
break;
default:
// MAV_FRAME_LOCAL_NED interpret as an offset from home
target_loc = rover.ahrs.get_home();
location_offset(target_loc, packet.x, packet.y);
break;
}
}
float target_speed = 0.0f;
float target_yaw_cd = 0.0f;
// consume velocity and convert to target speed and heading
if (!vel_ignore) {
const float speed_max = rover.control_mode->get_speed_default();
// convert vector length into a speed
target_speed = constrain_float(safe_sqrt(sq(packet.vx) + sq(packet.vy)), -speed_max, speed_max);
// convert vector direction to target yaw
target_yaw_cd = degrees(atan2f(packet.vy, packet.vx)) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw heading
if (!yaw_ignore) {
target_yaw_cd = ToDeg(packet.yaw) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw rate
float target_turn_rate_cds = 0.0f;
if (!yaw_rate_ignore) {
target_turn_rate_cds = ToDeg(packet.yaw_rate) * 100.0f;
}
// handling case when both velocity and either yaw or yaw-rate are provided
// by default, we consider that the rover will drive forward
float speed_dir = 1.0f;
if (!vel_ignore && (!yaw_ignore || !yaw_rate_ignore)) {
// Note: we are using the x-axis velocity to determine direction even though
// the frame may have been provided in MAV_FRAME_LOCAL_OFFSET_NED or MAV_FRAME_LOCAL_NED
if (is_negative(packet.vx)) {
speed_dir = -1.0f;
}
}
// set guided mode targets
if (!pos_ignore && vel_ignore && acc_ignore && yaw_ignore && yaw_rate_ignore) {
// consume position target
rover.mode_guided.set_desired_location(target_loc);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume velocity and turn rate
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume just target heading (probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, 0.0f);
} else if (pos_ignore && vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume just turn rate(probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, 0.0f);
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT: // MAV ID: 86
{
// decode packet
mavlink_set_position_target_global_int_t packet;
mavlink_msg_set_position_target_global_int_decode(msg, &packet);
// exit if vehicle is not in Guided mode
if (rover.control_mode != &rover.mode_guided) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_GLOBAL &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_INT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_RELATIVE_ALT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_RELATIVE_ALT_INT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_TERRAIN_ALT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_TERRAIN_ALT_INT) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
// prepare target position
Location target_loc = rover.current_loc;
if (!pos_ignore) {
// sanity check location
if (!check_latlng(packet.lat_int, packet.lon_int)) {
// result = MAV_RESULT_FAILED;
break;
}
target_loc.lat = packet.lat_int;
target_loc.lng = packet.lon_int;
}
float target_speed = 0.0f;
float target_yaw_cd = 0.0f;
// consume velocity and convert to target speed and heading
if (!vel_ignore) {
const float speed_max = rover.control_mode->get_speed_default();
// convert vector length into a speed
target_speed = constrain_float(safe_sqrt(sq(packet.vx) + sq(packet.vy)), -speed_max, speed_max);
// convert vector direction to target yaw
target_yaw_cd = degrees(atan2f(packet.vy, packet.vx)) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw heading
if (!yaw_ignore) {
target_yaw_cd = ToDeg(packet.yaw) * 100.0f;
// rotate target yaw if provided in body-frame
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
target_yaw_cd = wrap_180_cd(target_yaw_cd + rover.ahrs.yaw_sensor);
}
}
// consume yaw rate
float target_turn_rate_cds = 0.0f;
if (!yaw_rate_ignore) {
target_turn_rate_cds = ToDeg(packet.yaw_rate) * 100.0f;
}
// handling case when both velocity and either yaw or yaw-rate are provided
// by default, we consider that the rover will drive forward
float speed_dir = 1.0f;
if (!vel_ignore && (!yaw_ignore || !yaw_rate_ignore)) {
// Note: we are using the x-axis velocity to determine direction even though
// the frame is provided in MAV_FRAME_GLOBAL_xxx
if (is_negative(packet.vx)) {
speed_dir = -1.0f;
}
}
// set guided mode targets
if (!pos_ignore && vel_ignore && acc_ignore && yaw_ignore && yaw_rate_ignore) {
// consume position target
rover.mode_guided.set_desired_location(target_loc);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume velocity and turn rate
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, speed_dir * target_speed);
} else if (pos_ignore && !vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume velocity
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, speed_dir * target_speed);
} else if (pos_ignore && vel_ignore && acc_ignore && !yaw_ignore && yaw_rate_ignore) {
// consume just target heading (probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_heading_and_speed(target_yaw_cd, 0.0f);
} else if (pos_ignore && vel_ignore && acc_ignore && yaw_ignore && !yaw_rate_ignore) {
// consume just turn rate(probably only skid steering vehicles can do this)
rover.mode_guided.set_desired_turn_rate_and_speed(target_turn_rate_cds, 0.0f);
}
break;
}
#if HIL_MODE != HIL_MODE_DISABLED
case MAVLINK_MSG_ID_HIL_STATE:
{
mavlink_hil_state_t packet;
mavlink_msg_hil_state_decode(msg, &packet);
// sanity check location
if (!check_latlng(packet.lat, packet.lon)) {
break;
}
// set gps hil sensor
Location loc;
loc.lat = packet.lat;
loc.lng = packet.lon;
loc.alt = packet.alt/10;
Vector3f vel(packet.vx, packet.vy, packet.vz);
vel *= 0.01f;
gps.setHIL(0, AP_GPS::GPS_OK_FIX_3D,
packet.time_usec/1000,
loc, vel, 10, 0);
// rad/sec
Vector3f gyros;
gyros.x = packet.rollspeed;
gyros.y = packet.pitchspeed;
gyros.z = packet.yawspeed;
// m/s/s
Vector3f accels;
accels.x = packet.xacc * (GRAVITY_MSS/1000.0f);
accels.y = packet.yacc * (GRAVITY_MSS/1000.0f);
accels.z = packet.zacc * (GRAVITY_MSS/1000.0f);
ins.set_gyro(0, gyros);
ins.set_accel(0, accels);
compass.setHIL(0, packet.roll, packet.pitch, packet.yaw);
compass.setHIL(1, packet.roll, packet.pitch, packet.yaw);
break;
}
#endif // HIL_MODE
#if MOUNT == ENABLED
// deprecated. Use MAV_CMD_DO_MOUNT_CONFIGURE
case MAVLINK_MSG_ID_MOUNT_CONFIGURE:
{
rover.camera_mount.configure_msg(msg);
break;
}
// deprecated. Use MAV_CMD_DO_MOUNT_CONTROL
case MAVLINK_MSG_ID_MOUNT_CONTROL:
{
rover.camera_mount.control_msg(msg);
break;
}
#endif // MOUNT == ENABLED
case MAVLINK_MSG_ID_RADIO:
case MAVLINK_MSG_ID_RADIO_STATUS:
{
handle_radio_status(msg, rover.DataFlash, rover.should_log(MASK_LOG_PM));
break;
}
// send or receive fence points with GCS
case MAVLINK_MSG_ID_FENCE_POINT: // MAV ID: 160
case MAVLINK_MSG_ID_FENCE_FETCH_POINT:
rover.g2.fence.handle_msg(*this, msg);
break;
case MAVLINK_MSG_ID_DISTANCE_SENSOR:
rover.rangefinder.handle_msg(msg);
rover.g2.proximity.handle_msg(msg);
break;
default:
handle_common_message(msg);
break;
} // end switch
} // end handle mavlink
static void
handle_message(mavlink_message_t *msg)
{
if (msg->msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
mavlink_command_long_t cmd_mavlink;
mavlink_msg_command_long_decode(msg, &cmd_mavlink);
if (cmd_mavlink.target_system == mavlink_system.sysid && ((cmd_mavlink.target_component == mavlink_system.compid)
|| (cmd_mavlink.target_component == MAV_COMP_ID_ALL))) {
//check for MAVLINK terminate command
if (cmd_mavlink.command == MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN && ((int)cmd_mavlink.param1) == 3) {
/* This is the link shutdown command, terminate mavlink */
printf("[mavlink] Terminating .. \n");
fflush(stdout);
usleep(50000);
/* terminate other threads and this thread */
thread_should_exit = true;
} else {
/* Copy the content of mavlink_command_long_t cmd_mavlink into command_t cmd */
vcmd.param1 = cmd_mavlink.param1;
vcmd.param2 = cmd_mavlink.param2;
vcmd.param3 = cmd_mavlink.param3;
vcmd.param4 = cmd_mavlink.param4;
vcmd.param5 = cmd_mavlink.param5;
vcmd.param6 = cmd_mavlink.param6;
vcmd.param7 = cmd_mavlink.param7;
vcmd.command = cmd_mavlink.command;
vcmd.target_system = cmd_mavlink.target_system;
vcmd.target_component = cmd_mavlink.target_component;
vcmd.source_system = msg->sysid;
vcmd.source_component = msg->compid;
vcmd.confirmation = cmd_mavlink.confirmation;
/* check if topic is advertised */
if (cmd_pub <= 0) {
cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd);
}
/* publish */
orb_publish(ORB_ID(vehicle_command), cmd_pub, &vcmd);
}
}
}
if (msg->msgid == MAVLINK_MSG_ID_OPTICAL_FLOW) {
mavlink_optical_flow_t flow;
mavlink_msg_optical_flow_decode(msg, &flow);
struct optical_flow_s f;
f.timestamp = flow.time_usec;
f.flow_raw_x = flow.flow_x;
f.flow_raw_y = flow.flow_y;
f.flow_comp_x_m = flow.flow_comp_m_x;
f.flow_comp_y_m = flow.flow_comp_m_y;
f.ground_distance_m = flow.ground_distance;
f.quality = flow.quality;
f.sensor_id = flow.sensor_id;
/* check if topic is advertised */
if (flow_pub <= 0) {
flow_pub = orb_advertise(ORB_ID(optical_flow), &f);
} else {
/* publish */
orb_publish(ORB_ID(optical_flow), flow_pub, &f);
}
}
if (msg->msgid == MAVLINK_MSG_ID_SET_MODE) {
/* Set mode on request */
mavlink_set_mode_t new_mode;
mavlink_msg_set_mode_decode(msg, &new_mode);
/* Copy the content of mavlink_command_long_t cmd_mavlink into command_t cmd */
vcmd.param1 = new_mode.base_mode;
vcmd.param2 = new_mode.custom_mode;
vcmd.param3 = 0;
vcmd.param4 = 0;
vcmd.param5 = 0;
vcmd.param6 = 0;
vcmd.param7 = 0;
vcmd.command = MAV_CMD_DO_SET_MODE;
vcmd.target_system = new_mode.target_system;
vcmd.target_component = MAV_COMP_ID_ALL;
vcmd.source_system = msg->sysid;
vcmd.source_component = msg->compid;
vcmd.confirmation = 1;
/* check if topic is advertised */
if (cmd_pub <= 0) {
cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd);
} else {
/* create command */
orb_publish(ORB_ID(vehicle_command), cmd_pub, &vcmd);
}
}
/* Handle Vicon position estimates */
if (msg->msgid == MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE) {
mavlink_vicon_position_estimate_t pos;
mavlink_msg_vicon_position_estimate_decode(msg, &pos);
vicon_position.timestamp = hrt_absolute_time();
vicon_position.x = pos.x;
vicon_position.y = pos.y;
vicon_position.z = pos.z;
vicon_position.roll = pos.roll;
vicon_position.pitch = pos.pitch;
vicon_position.yaw = pos.yaw;
if (vicon_position_pub <= 0) {
vicon_position_pub = orb_advertise(ORB_ID(vehicle_vicon_position), &vicon_position);
} else {
orb_publish(ORB_ID(vehicle_vicon_position), vicon_position_pub, &vicon_position);
}
}
/* Handle quadrotor motor setpoints */
if (msg->msgid == MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST) {
mavlink_set_quad_swarm_roll_pitch_yaw_thrust_t quad_motors_setpoint;
mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust_decode(msg, &quad_motors_setpoint);
if (mavlink_system.sysid < 4) {
/* switch to a receiving link mode */
gcs_link = false;
/*
* rate control mode - defined by MAVLink
*/
uint8_t ml_mode = 0;
bool ml_armed = false;
switch (quad_motors_setpoint.mode) {
case 0:
ml_armed = false;
break;
case 1:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_RATES;
ml_armed = true;
break;
case 2:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE;
ml_armed = true;
break;
case 3:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_VELOCITY;
break;
case 4:
ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_POSITION;
break;
}
offboard_control_sp.p1 = (float)quad_motors_setpoint.roll[mavlink_system.sysid - 1] / (float)INT16_MAX;
offboard_control_sp.p2 = (float)quad_motors_setpoint.pitch[mavlink_system.sysid - 1] / (float)INT16_MAX;
offboard_control_sp.p3 = (float)quad_motors_setpoint.yaw[mavlink_system.sysid - 1] / (float)INT16_MAX;
offboard_control_sp.p4 = (float)quad_motors_setpoint.thrust[mavlink_system.sysid - 1] / (float)UINT16_MAX;
if (quad_motors_setpoint.thrust[mavlink_system.sysid - 1] == 0) {
ml_armed = false;
}
offboard_control_sp.armed = ml_armed;
offboard_control_sp.mode = ml_mode;
offboard_control_sp.timestamp = hrt_absolute_time();
/* check if topic has to be advertised */
if (offboard_control_sp_pub <= 0) {
offboard_control_sp_pub = orb_advertise(ORB_ID(offboard_control_setpoint), &offboard_control_sp);
} else {
/* Publish */
orb_publish(ORB_ID(offboard_control_setpoint), offboard_control_sp_pub, &offboard_control_sp);
}
}
}
/*
* Only decode hil messages in HIL mode.
*
* The HIL mode is enabled by the HIL bit flag
* in the system mode. Either send a set mode
* COMMAND_LONG message or a SET_MODE message
*/
if (mavlink_hil_enabled) {
uint64_t timestamp = hrt_absolute_time();
/* TODO, set ground_press/ temp during calib */
static const float ground_press = 1013.25f; // mbar
static const float ground_tempC = 21.0f;
static const float ground_alt = 0.0f;
static const float T0 = 273.15;
static const float R = 287.05f;
static const float g = 9.806f;
if (msg->msgid == MAVLINK_MSG_ID_RAW_IMU) {
mavlink_raw_imu_t imu;
mavlink_msg_raw_imu_decode(msg, &imu);
/* packet counter */
static uint16_t hil_counter = 0;
static uint16_t hil_frames = 0;
static uint64_t old_timestamp = 0;
/* sensors general */
hil_sensors.timestamp = imu.time_usec;
/* hil gyro */
static const float mrad2rad = 1.0e-3f;
hil_sensors.gyro_counter = hil_counter;
hil_sensors.gyro_raw[0] = imu.xgyro;
hil_sensors.gyro_raw[1] = imu.ygyro;
hil_sensors.gyro_raw[2] = imu.zgyro;
hil_sensors.gyro_rad_s[0] = imu.xgyro * mrad2rad;
hil_sensors.gyro_rad_s[1] = imu.ygyro * mrad2rad;
hil_sensors.gyro_rad_s[2] = imu.zgyro * mrad2rad;
/* accelerometer */
hil_sensors.accelerometer_counter = hil_counter;
static const float mg2ms2 = 9.8f / 1000.0f;
hil_sensors.accelerometer_raw[0] = imu.xacc;
hil_sensors.accelerometer_raw[1] = imu.yacc;
hil_sensors.accelerometer_raw[2] = imu.zacc;
hil_sensors.accelerometer_m_s2[0] = mg2ms2 * imu.xacc;
hil_sensors.accelerometer_m_s2[1] = mg2ms2 * imu.yacc;
hil_sensors.accelerometer_m_s2[2] = mg2ms2 * imu.zacc;
hil_sensors.accelerometer_mode = 0; // TODO what is this?
hil_sensors.accelerometer_range_m_s2 = 32.7f; // int16
/* adc */
hil_sensors.adc_voltage_v[0] = 0;
hil_sensors.adc_voltage_v[1] = 0;
hil_sensors.adc_voltage_v[2] = 0;
/* magnetometer */
float mga2ga = 1.0e-3f;
hil_sensors.magnetometer_counter = hil_counter;
hil_sensors.magnetometer_raw[0] = imu.xmag;
hil_sensors.magnetometer_raw[1] = imu.ymag;
hil_sensors.magnetometer_raw[2] = imu.zmag;
hil_sensors.magnetometer_ga[0] = imu.xmag * mga2ga;
hil_sensors.magnetometer_ga[1] = imu.ymag * mga2ga;
hil_sensors.magnetometer_ga[2] = imu.zmag * mga2ga;
hil_sensors.magnetometer_range_ga = 32.7f; // int16
hil_sensors.magnetometer_mode = 0; // TODO what is this
hil_sensors.magnetometer_cuttoff_freq_hz = 50.0f;
/* publish */
orb_publish(ORB_ID(sensor_combined), pub_hil_sensors, &hil_sensors);
// increment counters
hil_counter += 1 ;
hil_frames += 1 ;
// output
if ((timestamp - old_timestamp) > 10000000) {
printf("receiving hil imu at %d hz\n", hil_frames/10);
old_timestamp = timestamp;
hil_frames = 0;
}
}
if (msg->msgid == MAVLINK_MSG_ID_HIGHRES_IMU) {
mavlink_highres_imu_t imu;
mavlink_msg_highres_imu_decode(msg, &imu);
/* packet counter */
static uint16_t hil_counter = 0;
static uint16_t hil_frames = 0;
static uint64_t old_timestamp = 0;
/* sensors general */
hil_sensors.timestamp = imu.time_usec;
/* hil gyro */
static const float mrad2rad = 1.0e-3f;
hil_sensors.gyro_counter = hil_counter;
hil_sensors.gyro_raw[0] = imu.xgyro / mrad2rad;
hil_sensors.gyro_raw[1] = imu.ygyro / mrad2rad;
hil_sensors.gyro_raw[2] = imu.zgyro / mrad2rad;
hil_sensors.gyro_rad_s[0] = imu.xgyro;
hil_sensors.gyro_rad_s[1] = imu.ygyro;
hil_sensors.gyro_rad_s[2] = imu.zgyro;
/* accelerometer */
hil_sensors.accelerometer_counter = hil_counter;
static const float mg2ms2 = 9.8f / 1000.0f;
hil_sensors.accelerometer_raw[0] = imu.xacc / mg2ms2;
hil_sensors.accelerometer_raw[1] = imu.yacc / mg2ms2;
hil_sensors.accelerometer_raw[2] = imu.zacc / mg2ms2;
hil_sensors.accelerometer_m_s2[0] = imu.xacc;
hil_sensors.accelerometer_m_s2[1] = imu.yacc;
hil_sensors.accelerometer_m_s2[2] = imu.zacc;
hil_sensors.accelerometer_mode = 0; // TODO what is this?
hil_sensors.accelerometer_range_m_s2 = 32.7f; // int16
/* adc */
hil_sensors.adc_voltage_v[0] = 0;
hil_sensors.adc_voltage_v[1] = 0;
hil_sensors.adc_voltage_v[2] = 0;
/* magnetometer */
float mga2ga = 1.0e-3f;
hil_sensors.magnetometer_counter = hil_counter;
hil_sensors.magnetometer_raw[0] = imu.xmag / mga2ga;
hil_sensors.magnetometer_raw[1] = imu.ymag / mga2ga;
hil_sensors.magnetometer_raw[2] = imu.zmag / mga2ga;
hil_sensors.magnetometer_ga[0] = imu.xmag;
hil_sensors.magnetometer_ga[1] = imu.ymag;
hil_sensors.magnetometer_ga[2] = imu.zmag;
hil_sensors.magnetometer_range_ga = 32.7f; // int16
hil_sensors.magnetometer_mode = 0; // TODO what is this
hil_sensors.magnetometer_cuttoff_freq_hz = 50.0f;
hil_sensors.baro_pres_mbar = imu.abs_pressure;
float tempC = imu.temperature;
float tempAvgK = T0 + (tempC + ground_tempC) / 2.0f;
float h = ground_alt + (R / g) * tempAvgK * logf(ground_press / imu.abs_pressure);
hil_sensors.baro_alt_meter = h;
hil_sensors.baro_temp_celcius = imu.temperature;
/* publish */
orb_publish(ORB_ID(sensor_combined), pub_hil_sensors, &hil_sensors);
// increment counters
hil_counter += 1 ;
hil_frames += 1 ;
// output
if ((timestamp - old_timestamp) > 10000000) {
printf("receiving hil imu at %d hz\n", hil_frames/10);
old_timestamp = timestamp;
hil_frames = 0;
}
}
if (msg->msgid == MAVLINK_MSG_ID_GPS_RAW_INT) {
mavlink_gps_raw_int_t gps;
mavlink_msg_gps_raw_int_decode(msg, &gps);
/* packet counter */
static uint16_t hil_counter = 0;
static uint16_t hil_frames = 0;
static uint64_t old_timestamp = 0;
/* gps */
hil_gps.timestamp_position = gps.time_usec;
// hil_gps.counter = hil_counter++;
hil_gps.time_gps_usec = gps.time_usec;
hil_gps.lat = gps.lat;
hil_gps.lon = gps.lon;
hil_gps.alt = gps.alt;
// hil_gps.counter_pos_valid = hil_counter++;
hil_gps.eph_m = (float)gps.eph * 1e-2f; // from cm to m
hil_gps.epv_m = (float)gps.epv * 1e-2f; // from cm to m
hil_gps.s_variance_m_s = 100; // XXX 100 m/s variance?
hil_gps.p_variance_m = 100; // XXX 100 m variance?
hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
hil_gps.vel_n_m_s = (float)gps.vel * 1e-2f * cosf(gps.cog * M_DEG_TO_RAD_F * 1e-2f);
hil_gps.vel_e_m_s = (float)gps.vel * 1e-2f * sinf(gps.cog * M_DEG_TO_RAD_F * 1e-2f);
hil_gps.vel_d_m_s = 0.0f;
hil_gps.cog_rad = gps.cog * M_DEG_TO_RAD_F * 1e-2f; // from deg*100 to rad
hil_gps.fix_type = gps.fix_type;
hil_gps.satellites_visible = gps.satellites_visible;
/* publish */
orb_publish(ORB_ID(vehicle_gps_position), pub_hil_gps, &hil_gps);
// increment counters
hil_counter += 1 ;
hil_frames += 1 ;
// output
if ((timestamp - old_timestamp) > 10000000) {
printf("receiving hil gps at %d hz\n", hil_frames/10);
old_timestamp = timestamp;
hil_frames = 0;
}
}
if (msg->msgid == MAVLINK_MSG_ID_RAW_PRESSURE) {
mavlink_raw_pressure_t press;
mavlink_msg_raw_pressure_decode(msg, &press);
/* packet counter */
static uint16_t hil_counter = 0;
static uint16_t hil_frames = 0;
static uint64_t old_timestamp = 0;
/* sensors general */
hil_sensors.timestamp = press.time_usec;
/* baro */
float tempC = press.temperature / 100.0f;
float tempAvgK = T0 + (tempC + ground_tempC) / 2.0f;
float h = ground_alt + (R / g) * tempAvgK * logf(ground_press / press.press_abs);
hil_sensors.baro_counter = hil_counter;
hil_sensors.baro_pres_mbar = press.press_abs;
hil_sensors.baro_alt_meter = h;
hil_sensors.baro_temp_celcius = tempC;
/* publish */
orb_publish(ORB_ID(sensor_combined), pub_hil_sensors, &hil_sensors);
// increment counters
hil_counter += 1 ;
hil_frames += 1 ;
// output
if ((timestamp - old_timestamp) > 10000000) {
printf("receiving hil pressure at %d hz\n", hil_frames/10);
old_timestamp = timestamp;
hil_frames = 0;
}
}
if (msg->msgid == MAVLINK_MSG_ID_HIL_STATE) {
mavlink_hil_state_t hil_state;
mavlink_msg_hil_state_decode(msg, &hil_state);
/* Calculate Rotation Matrix */
//TODO: better clarification which app does this, atm we have a ekf for quadrotors which does this, but there is no such thing if fly in fixed wing mode
if (mavlink_system.type == MAV_TYPE_FIXED_WING) {
//TODO: assuming low pitch and roll values for now
hil_attitude.R[0][0] = cosf(hil_state.yaw);
hil_attitude.R[0][1] = sinf(hil_state.yaw);
hil_attitude.R[0][2] = 0.0f;
hil_attitude.R[1][0] = -sinf(hil_state.yaw);
hil_attitude.R[1][1] = cosf(hil_state.yaw);
hil_attitude.R[1][2] = 0.0f;
hil_attitude.R[2][0] = 0.0f;
hil_attitude.R[2][1] = 0.0f;
hil_attitude.R[2][2] = 1.0f;
hil_attitude.R_valid = true;
}
hil_global_pos.lat = hil_state.lat;
hil_global_pos.lon = hil_state.lon;
hil_global_pos.alt = hil_state.alt / 1000.0f;
hil_global_pos.vx = hil_state.vx / 100.0f;
hil_global_pos.vy = hil_state.vy / 100.0f;
hil_global_pos.vz = hil_state.vz / 100.0f;
/* set timestamp and notify processes (broadcast) */
hil_global_pos.timestamp = hrt_absolute_time();
orb_publish(ORB_ID(vehicle_global_position), pub_hil_global_pos, &hil_global_pos);
hil_attitude.roll = hil_state.roll;
hil_attitude.pitch = hil_state.pitch;
hil_attitude.yaw = hil_state.yaw;
hil_attitude.rollspeed = hil_state.rollspeed;
hil_attitude.pitchspeed = hil_state.pitchspeed;
hil_attitude.yawspeed = hil_state.yawspeed;
/* set timestamp and notify processes (broadcast) */
hil_attitude.timestamp = hrt_absolute_time();
orb_publish(ORB_ID(vehicle_attitude), pub_hil_attitude, &hil_attitude);
}
if (msg->msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) {
mavlink_manual_control_t man;
mavlink_msg_manual_control_decode(msg, &man);
struct rc_channels_s rc_hil;
memset(&rc_hil, 0, sizeof(rc_hil));
static orb_advert_t rc_pub = 0;
rc_hil.timestamp = hrt_absolute_time();
rc_hil.chan_count = 4;
rc_hil.chan[0].scaled = man.x / 1000.0f;
rc_hil.chan[1].scaled = man.y / 1000.0f;
rc_hil.chan[2].scaled = man.r / 1000.0f;
rc_hil.chan[3].scaled = man.z / 1000.0f;
struct manual_control_setpoint_s mc;
static orb_advert_t mc_pub = 0;
int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
/* get a copy first, to prevent altering values that are not sent by the mavlink command */
orb_copy(ORB_ID(manual_control_setpoint), manual_sub, &mc);
mc.timestamp = rc_hil.timestamp;
mc.roll = man.x / 1000.0f;
mc.pitch = man.y / 1000.0f;
mc.yaw = man.r / 1000.0f;
mc.throttle = man.z / 1000.0f;
/* fake RC channels with manual control input from simulator */
if (rc_pub == 0) {
rc_pub = orb_advertise(ORB_ID(rc_channels), &rc_hil);
} else {
orb_publish(ORB_ID(rc_channels), rc_pub, &rc_hil);
}
if (mc_pub == 0) {
mc_pub = orb_advertise(ORB_ID(manual_control_setpoint), &mc);
} else {
orb_publish(ORB_ID(manual_control_setpoint), mc_pub, &mc);
}
}
}
}
void GCS_MAVLINK_Copter::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
case MAVLINK_MSG_ID_HEARTBEAT: // MAV ID: 0
{
// We keep track of the last time we received a heartbeat from our GCS for failsafe purposes
if(msg->sysid != copter.g.sysid_my_gcs) break;
copter.failsafe.last_heartbeat_ms = AP_HAL::millis();
break;
}
case MAVLINK_MSG_ID_MANUAL_CONTROL:
{
if (msg->sysid != copter.g.sysid_my_gcs) {
break; // only accept control from our gcs
}
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
if (packet.target != copter.g.sysid_this_mav) {
break; // only accept control aimed at us
}
if (packet.z < 0) { // Copter doesn't do negative thrust
break;
}
uint32_t tnow = AP_HAL::millis();
manual_override(copter.channel_roll, packet.y, 1000, 2000, tnow);
manual_override(copter.channel_pitch, packet.x, 1000, 2000, tnow, true);
manual_override(copter.channel_throttle, packet.z, 0, 1000, tnow);
manual_override(copter.channel_yaw, packet.r, 1000, 2000, tnow);
// a manual control message is considered to be a 'heartbeat' from the ground station for failsafe purposes
copter.failsafe.last_heartbeat_ms = tnow;
break;
}
#if MODE_GUIDED_ENABLED == ENABLED
case MAVLINK_MSG_ID_SET_ATTITUDE_TARGET: // MAV ID: 82
{
// decode packet
mavlink_set_attitude_target_t packet;
mavlink_msg_set_attitude_target_decode(msg, &packet);
// exit if vehicle is not in Guided mode or Auto-Guided mode
if (!copter.flightmode->in_guided_mode()) {
break;
}
// ensure type_mask specifies to use attitude and thrust
if ((packet.type_mask & ((1<<7)|(1<<6))) != 0) {
break;
}
// convert thrust to climb rate
packet.thrust = constrain_float(packet.thrust, 0.0f, 1.0f);
float climb_rate_cms = 0.0f;
if (is_equal(packet.thrust, 0.5f)) {
climb_rate_cms = 0.0f;
} else if (packet.thrust > 0.5f) {
// climb at up to WPNAV_SPEED_UP
climb_rate_cms = (packet.thrust - 0.5f) * 2.0f * copter.wp_nav->get_default_speed_up();
} else {
// descend at up to WPNAV_SPEED_DN
climb_rate_cms = (0.5f - packet.thrust) * 2.0f * -fabsf(copter.wp_nav->get_default_speed_down());
}
// if the body_yaw_rate field is ignored, use the commanded yaw position
// otherwise use the commanded yaw rate
bool use_yaw_rate = false;
if ((packet.type_mask & (1<<2)) == 0) {
use_yaw_rate = true;
}
copter.mode_guided.set_angle(Quaternion(packet.q[0],packet.q[1],packet.q[2],packet.q[3]),
climb_rate_cms, use_yaw_rate, packet.body_yaw_rate);
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED: // MAV ID: 84
{
// decode packet
mavlink_set_position_target_local_ned_t packet;
mavlink_msg_set_position_target_local_ned_decode(msg, &packet);
// exit if vehicle is not in Guided mode or Auto-Guided mode
if (!copter.flightmode->in_guided_mode()) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_LOCAL_NED &&
packet.coordinate_frame != MAV_FRAME_LOCAL_OFFSET_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_OFFSET_NED) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
/*
* for future use:
* bool force = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_FORCE;
*/
// prepare position
Vector3f pos_vector;
if (!pos_ignore) {
// convert to cm
pos_vector = Vector3f(packet.x * 100.0f, packet.y * 100.0f, -packet.z * 100.0f);
// rotate to body-frame if necessary
if (packet.coordinate_frame == MAV_FRAME_BODY_NED ||
packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
copter.rotate_body_frame_to_NE(pos_vector.x, pos_vector.y);
}
// add body offset if necessary
if (packet.coordinate_frame == MAV_FRAME_LOCAL_OFFSET_NED ||
packet.coordinate_frame == MAV_FRAME_BODY_NED ||
packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
pos_vector += copter.inertial_nav.get_position();
} else {
// convert from alt-above-home to alt-above-ekf-origin
if (!AP::ahrs().home_is_set()) {
break;
}
const Location &origin = copter.inertial_nav.get_origin();
pos_vector.z += AP::ahrs().get_home().alt;
pos_vector.z -= origin.alt;
}
}
// prepare velocity
Vector3f vel_vector;
if (!vel_ignore) {
// convert to cm
vel_vector = Vector3f(packet.vx * 100.0f, packet.vy * 100.0f, -packet.vz * 100.0f);
// rotate to body-frame if necessary
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
copter.rotate_body_frame_to_NE(vel_vector.x, vel_vector.y);
}
}
// prepare yaw
float yaw_cd = 0.0f;
bool yaw_relative = false;
float yaw_rate_cds = 0.0f;
if (!yaw_ignore) {
yaw_cd = ToDeg(packet.yaw) * 100.0f;
yaw_relative = packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED;
}
if (!yaw_rate_ignore) {
yaw_rate_cds = ToDeg(packet.yaw_rate) * 100.0f;
}
// send request
if (!pos_ignore && !vel_ignore && acc_ignore) {
copter.mode_guided.set_destination_posvel(pos_vector, vel_vector, !yaw_ignore, yaw_cd, !yaw_rate_ignore, yaw_rate_cds, yaw_relative);
} else if (pos_ignore && !vel_ignore && acc_ignore) {
copter.mode_guided.set_velocity(vel_vector, !yaw_ignore, yaw_cd, !yaw_rate_ignore, yaw_rate_cds, yaw_relative);
} else if (!pos_ignore && vel_ignore && acc_ignore) {
copter.mode_guided.set_destination(pos_vector, !yaw_ignore, yaw_cd, !yaw_rate_ignore, yaw_rate_cds, yaw_relative);
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT: // MAV ID: 86
{
// decode packet
mavlink_set_position_target_global_int_t packet;
mavlink_msg_set_position_target_global_int_decode(msg, &packet);
// exit if vehicle is not in Guided mode or Auto-Guided mode
if (!copter.flightmode->in_guided_mode()) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
/*
* for future use:
* bool force = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_FORCE;
*/
Vector3f pos_neu_cm; // position (North, East, Up coordinates) in centimeters
if(!pos_ignore) {
// sanity check location
if (!check_latlng(packet.lat_int, packet.lon_int)) {
break;
}
Location::AltFrame frame;
if (!mavlink_coordinate_frame_to_location_alt_frame(packet.coordinate_frame, frame)) {
// unknown coordinate frame
break;
}
const Location loc{
packet.lat_int,
packet.lon_int,
int32_t(packet.alt*100),
frame,
};
if (!loc.get_vector_from_origin_NEU(pos_neu_cm)) {
break;
}
}
// prepare yaw
float yaw_cd = 0.0f;
bool yaw_relative = false;
float yaw_rate_cds = 0.0f;
if (!yaw_ignore) {
yaw_cd = ToDeg(packet.yaw) * 100.0f;
yaw_relative = packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED;
}
if (!yaw_rate_ignore) {
yaw_rate_cds = ToDeg(packet.yaw_rate) * 100.0f;
}
if (!pos_ignore && !vel_ignore && acc_ignore) {
copter.mode_guided.set_destination_posvel(pos_neu_cm, Vector3f(packet.vx * 100.0f, packet.vy * 100.0f, -packet.vz * 100.0f), !yaw_ignore, yaw_cd, !yaw_rate_ignore, yaw_rate_cds, yaw_relative);
} else if (pos_ignore && !vel_ignore && acc_ignore) {
copter.mode_guided.set_velocity(Vector3f(packet.vx * 100.0f, packet.vy * 100.0f, -packet.vz * 100.0f), !yaw_ignore, yaw_cd, !yaw_rate_ignore, yaw_rate_cds, yaw_relative);
} else if (!pos_ignore && vel_ignore && acc_ignore) {
copter.mode_guided.set_destination(pos_neu_cm, !yaw_ignore, yaw_cd, !yaw_rate_ignore, yaw_rate_cds, yaw_relative);
}
break;
}
#endif
case MAVLINK_MSG_ID_DISTANCE_SENSOR:
{
copter.rangefinder.handle_msg(msg);
#if PROXIMITY_ENABLED == ENABLED
copter.g2.proximity.handle_msg(msg);
#endif
break;
}
case MAVLINK_MSG_ID_OBSTACLE_DISTANCE:
{
#if PROXIMITY_ENABLED == ENABLED
copter.g2.proximity.handle_msg(msg);
#endif
break;
}
#if HIL_MODE != HIL_MODE_DISABLED
case MAVLINK_MSG_ID_HIL_STATE: // MAV ID: 90
{
mavlink_hil_state_t packet;
mavlink_msg_hil_state_decode(msg, &packet);
// sanity check location
if (!check_latlng(packet.lat, packet.lon)) {
break;
}
// set gps hil sensor
Location loc;
loc.lat = packet.lat;
loc.lng = packet.lon;
loc.alt = packet.alt/10;
Vector3f vel(packet.vx, packet.vy, packet.vz);
vel *= 0.01f;
gps.setHIL(0, AP_GPS::GPS_OK_FIX_3D,
packet.time_usec/1000,
loc, vel, 10, 0);
// rad/sec
Vector3f gyros;
gyros.x = packet.rollspeed;
gyros.y = packet.pitchspeed;
gyros.z = packet.yawspeed;
// m/s/s
Vector3f accels;
accels.x = packet.xacc * (GRAVITY_MSS/1000.0f);
accels.y = packet.yacc * (GRAVITY_MSS/1000.0f);
accels.z = packet.zacc * (GRAVITY_MSS/1000.0f);
ins.set_gyro(0, gyros);
ins.set_accel(0, accels);
AP::baro().setHIL(packet.alt*0.001f);
copter.compass.setHIL(0, packet.roll, packet.pitch, packet.yaw);
copter.compass.setHIL(1, packet.roll, packet.pitch, packet.yaw);
break;
}
#endif // HIL_MODE != HIL_MODE_DISABLED
case MAVLINK_MSG_ID_RADIO:
case MAVLINK_MSG_ID_RADIO_STATUS: // MAV ID: 109
{
handle_radio_status(msg, copter.should_log(MASK_LOG_PM));
break;
}
#if PRECISION_LANDING == ENABLED
case MAVLINK_MSG_ID_LANDING_TARGET:
copter.precland.handle_msg(msg);
break;
#endif
case MAVLINK_MSG_ID_TERRAIN_DATA:
case MAVLINK_MSG_ID_TERRAIN_CHECK:
#if AP_TERRAIN_AVAILABLE && AC_TERRAIN
copter.terrain.handle_data(chan, msg);
#endif
break;
case MAVLINK_MSG_ID_SET_HOME_POSITION:
{
mavlink_set_home_position_t packet;
mavlink_msg_set_home_position_decode(msg, &packet);
if((packet.latitude == 0) && (packet.longitude == 0) && (packet.altitude == 0)) {
if (!copter.set_home_to_current_location(true)) {
// silently ignored
}
} else {
Location new_home_loc;
new_home_loc.lat = packet.latitude;
new_home_loc.lng = packet.longitude;
new_home_loc.alt = packet.altitude / 10;
if (!copter.set_home(new_home_loc, true)) {
// silently ignored
}
}
break;
}
case MAVLINK_MSG_ID_ADSB_VEHICLE:
case MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_CFG:
case MAVLINK_MSG_ID_UAVIONIX_ADSB_OUT_DYNAMIC:
case MAVLINK_MSG_ID_UAVIONIX_ADSB_TRANSCEIVER_HEALTH_REPORT:
#if ADSB_ENABLED == ENABLED
copter.adsb.handle_message(chan, msg);
#endif
break;
#if TOY_MODE_ENABLED == ENABLED
case MAVLINK_MSG_ID_NAMED_VALUE_INT:
copter.g2.toy_mode.handle_message(msg);
break;
#endif
default:
handle_common_message(msg);
break;
} // end switch
} // end handle mavlink
void GCS_MAVLINK_Sub::handleMessage(mavlink_message_t* msg)
{
switch (msg->msgid) {
case MAVLINK_MSG_ID_HEARTBEAT: { // MAV ID: 0
// We keep track of the last time we received a heartbeat from our GCS for failsafe purposes
if (msg->sysid != sub.g.sysid_my_gcs) {
break;
}
sub.failsafe.last_heartbeat_ms = AP_HAL::millis();
break;
}
case MAVLINK_MSG_ID_MANUAL_CONTROL: { // MAV ID: 69
if (msg->sysid != sub.g.sysid_my_gcs) {
break; // Only accept control from our gcs
}
mavlink_manual_control_t packet;
mavlink_msg_manual_control_decode(msg, &packet);
if (packet.target != sub.g.sysid_this_mav) {
break; // only accept control aimed at us
}
sub.transform_manual_control_to_rc_override(packet.x,packet.y,packet.z,packet.r,packet.buttons);
sub.failsafe.last_pilot_input_ms = AP_HAL::millis();
// a RC override message is considered to be a 'heartbeat' from the ground station for failsafe purposes
sub.failsafe.last_heartbeat_ms = AP_HAL::millis();
break;
}
case MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE: { // MAV ID: 70
// allow override of RC input
if (msg->sysid != sub.g.sysid_my_gcs) {
break; // Only accept control from our gcs
}
uint32_t tnow = AP_HAL::millis();
mavlink_rc_channels_override_t packet;
mavlink_msg_rc_channels_override_decode(msg, &packet);
RC_Channels::set_override(0, packet.chan1_raw, tnow);
RC_Channels::set_override(1, packet.chan2_raw, tnow);
RC_Channels::set_override(2, packet.chan3_raw, tnow);
RC_Channels::set_override(3, packet.chan4_raw, tnow);
RC_Channels::set_override(4, packet.chan5_raw, tnow);
RC_Channels::set_override(5, packet.chan6_raw, tnow);
RC_Channels::set_override(6, packet.chan7_raw, tnow);
RC_Channels::set_override(7, packet.chan8_raw, tnow);
sub.failsafe.last_pilot_input_ms = tnow;
// a RC override message is considered to be a 'heartbeat' from the ground station for failsafe purposes
sub.failsafe.last_heartbeat_ms = tnow;
break;
}
case MAVLINK_MSG_ID_SET_ATTITUDE_TARGET: { // MAV ID: 82
// decode packet
mavlink_set_attitude_target_t packet;
mavlink_msg_set_attitude_target_decode(msg, &packet);
// ensure type_mask specifies to use attitude
// the thrust can be used from the altitude hold
if (packet.type_mask & (1<<6)) {
sub.set_attitude_target_no_gps = {AP_HAL::millis(), packet};
}
// ensure type_mask specifies to use attitude and thrust
if ((packet.type_mask & ((1<<7)|(1<<6))) != 0) {
break;
}
// convert thrust to climb rate
packet.thrust = constrain_float(packet.thrust, 0.0f, 1.0f);
float climb_rate_cms = 0.0f;
if (is_equal(packet.thrust, 0.5f)) {
climb_rate_cms = 0.0f;
} else if (packet.thrust > 0.5f) {
// climb at up to WPNAV_SPEED_UP
climb_rate_cms = (packet.thrust - 0.5f) * 2.0f * sub.wp_nav.get_default_speed_up();
} else {
// descend at up to WPNAV_SPEED_DN
climb_rate_cms = (packet.thrust - 0.5f) * 2.0f * fabsf(sub.wp_nav.get_default_speed_down());
}
sub.guided_set_angle(Quaternion(packet.q[0],packet.q[1],packet.q[2],packet.q[3]), climb_rate_cms);
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED: { // MAV ID: 84
// decode packet
mavlink_set_position_target_local_ned_t packet;
mavlink_msg_set_position_target_local_ned_decode(msg, &packet);
// exit if vehicle is not in Guided mode or Auto-Guided mode
if ((sub.control_mode != GUIDED) && !(sub.control_mode == AUTO && sub.auto_mode == Auto_NavGuided)) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_LOCAL_NED &&
packet.coordinate_frame != MAV_FRAME_LOCAL_OFFSET_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_NED &&
packet.coordinate_frame != MAV_FRAME_BODY_OFFSET_NED) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
/*
* for future use:
* bool force = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_FORCE;
* bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
* bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
*/
// prepare position
Vector3f pos_vector;
if (!pos_ignore) {
// convert to cm
pos_vector = Vector3f(packet.x * 100.0f, packet.y * 100.0f, -packet.z * 100.0f);
// rotate to body-frame if necessary
if (packet.coordinate_frame == MAV_FRAME_BODY_NED ||
packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
sub.rotate_body_frame_to_NE(pos_vector.x, pos_vector.y);
}
// add body offset if necessary
if (packet.coordinate_frame == MAV_FRAME_LOCAL_OFFSET_NED ||
packet.coordinate_frame == MAV_FRAME_BODY_NED ||
packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
pos_vector += sub.inertial_nav.get_position();
} else {
// convert from alt-above-home to alt-above-ekf-origin
pos_vector.z = sub.pv_alt_above_origin(pos_vector.z);
}
}
// prepare velocity
Vector3f vel_vector;
if (!vel_ignore) {
// convert to cm
vel_vector = Vector3f(packet.vx * 100.0f, packet.vy * 100.0f, -packet.vz * 100.0f);
// rotate to body-frame if necessary
if (packet.coordinate_frame == MAV_FRAME_BODY_NED || packet.coordinate_frame == MAV_FRAME_BODY_OFFSET_NED) {
sub.rotate_body_frame_to_NE(vel_vector.x, vel_vector.y);
}
}
// send request
if (!pos_ignore && !vel_ignore && acc_ignore) {
sub.guided_set_destination_posvel(pos_vector, vel_vector);
} else if (pos_ignore && !vel_ignore && acc_ignore) {
sub.guided_set_velocity(vel_vector);
} else if (!pos_ignore && vel_ignore && acc_ignore) {
sub.guided_set_destination(pos_vector);
}
break;
}
case MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT: { // MAV ID: 86
// decode packet
mavlink_set_position_target_global_int_t packet;
mavlink_msg_set_position_target_global_int_decode(msg, &packet);
// exit if vehicle is not in Guided mode or Auto-Guided mode
if ((sub.control_mode != GUIDED) && !(sub.control_mode == AUTO && sub.auto_mode == Auto_NavGuided)) {
break;
}
// check for supported coordinate frames
if (packet.coordinate_frame != MAV_FRAME_GLOBAL &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_INT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_RELATIVE_ALT && // solo shot manager incorrectly sends RELATIVE_ALT instead of RELATIVE_ALT_INT
packet.coordinate_frame != MAV_FRAME_GLOBAL_RELATIVE_ALT_INT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_TERRAIN_ALT &&
packet.coordinate_frame != MAV_FRAME_GLOBAL_TERRAIN_ALT_INT) {
break;
}
bool pos_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE;
bool vel_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE;
bool acc_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE;
/*
* for future use:
* bool force = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_FORCE;
* bool yaw_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE;
* bool yaw_rate_ignore = packet.type_mask & MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE;
*/
Vector3f pos_neu_cm; // position (North, East, Up coordinates) in centimeters
if (!pos_ignore) {
// sanity check location
if (!check_latlng(packet.lat_int, packet.lon_int)) {
break;
}
Location loc;
loc.lat = packet.lat_int;
loc.lng = packet.lon_int;
loc.alt = packet.alt*100;
switch (packet.coordinate_frame) {
case MAV_FRAME_GLOBAL_RELATIVE_ALT: // solo shot manager incorrectly sends RELATIVE_ALT instead of RELATIVE_ALT_INT
case MAV_FRAME_GLOBAL_RELATIVE_ALT_INT:
loc.relative_alt = true;
loc.terrain_alt = false;
break;
case MAV_FRAME_GLOBAL_TERRAIN_ALT:
case MAV_FRAME_GLOBAL_TERRAIN_ALT_INT:
loc.relative_alt = true;
loc.terrain_alt = true;
break;
case MAV_FRAME_GLOBAL:
case MAV_FRAME_GLOBAL_INT:
default:
loc.relative_alt = false;
loc.terrain_alt = false;
break;
}
pos_neu_cm = sub.pv_location_to_vector(loc);
}
if (!pos_ignore && !vel_ignore && acc_ignore) {
sub.guided_set_destination_posvel(pos_neu_cm, Vector3f(packet.vx * 100.0f, packet.vy * 100.0f, -packet.vz * 100.0f));
} else if (pos_ignore && !vel_ignore && acc_ignore) {
sub.guided_set_velocity(Vector3f(packet.vx * 100.0f, packet.vy * 100.0f, -packet.vz * 100.0f));
} else if (!pos_ignore && vel_ignore && acc_ignore) {
sub.guided_set_destination(pos_neu_cm);
}
break;
}
case MAVLINK_MSG_ID_DISTANCE_SENSOR: {
sub.rangefinder.handle_msg(msg);
break;
}
#if AC_FENCE == ENABLED
// send or receive fence points with GCS
case MAVLINK_MSG_ID_FENCE_POINT: // MAV ID: 160
case MAVLINK_MSG_ID_FENCE_FETCH_POINT:
sub.fence.handle_msg(*this, msg);
break;
#endif // AC_FENCE == ENABLED
case MAVLINK_MSG_ID_TERRAIN_DATA:
case MAVLINK_MSG_ID_TERRAIN_CHECK:
#if AP_TERRAIN_AVAILABLE && AC_TERRAIN
sub.terrain.handle_data(chan, msg);
#endif
break;
case MAVLINK_MSG_ID_SET_HOME_POSITION: {
mavlink_set_home_position_t packet;
mavlink_msg_set_home_position_decode(msg, &packet);
if ((packet.latitude == 0) && (packet.longitude == 0) && (packet.altitude == 0)) {
sub.set_home_to_current_location(true);
} else {
// sanity check location
if (!check_latlng(packet.latitude, packet.longitude)) {
break;
}
Location new_home_loc;
new_home_loc.lat = packet.latitude;
new_home_loc.lng = packet.longitude;
new_home_loc.alt = packet.altitude / 10;
if (sub.far_from_EKF_origin(new_home_loc)) {
break;
}
sub.set_home(new_home_loc, true);
}
break;
}
// This adds support for leak detectors in a separate enclosure
// connected to a mavlink enabled subsystem
case MAVLINK_MSG_ID_SYS_STATUS: {
uint32_t MAV_SENSOR_WATER = 0x20000000;
mavlink_sys_status_t packet;
mavlink_msg_sys_status_decode(msg, &packet);
if ((packet.onboard_control_sensors_enabled & MAV_SENSOR_WATER) && !(packet.onboard_control_sensors_health & MAV_SENSOR_WATER)) {
sub.leak_detector.set_detect();
}
}
break;
default:
handle_common_message(msg);
break;
} // end switch
} // end handle mavlink
