void MavlinkReceiver::handle_message_vicon_position_estimate(mavlink_message_t *msg) { mavlink_vicon_position_estimate_t pos; mavlink_msg_vicon_position_estimate_decode(msg, &pos); struct vehicle_vicon_position_s vicon_position; memset(&vicon_position, 0, sizeof(vicon_position)); 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); } }
//@{ void handle_mavlink_message(mavlink_channel_t chan, mavlink_message_t* msg) { uint8_t buf[MAVLINK_MAX_PACKET_LEN]; uint32_t len; switch (chan) { case MAVLINK_COMM_0: { if (msg->msgid != MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE) { // Copy to COMM 1 len = mavlink_msg_to_send_buffer(buf, msg); for (int i = 0; i < len; i++) { uart1_transmit(buf[i]); } } } break; case MAVLINK_COMM_1: { if (msg->msgid != MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE && msg->msgid != MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE) { // Copy to COMM 0 len = mavlink_msg_to_send_buffer(buf, msg); for (int i = 0; i < len; i++) { uart0_transmit(buf[i]); } break; } } default: break; } switch (msg->msgid) { case MAVLINK_MSG_ID_SET_MODE: { mavlink_set_mode_t mode; mavlink_msg_set_mode_decode(msg, &mode); // Check if this system should change the mode if (mode.target == (uint8_t)global_data.param[PARAM_SYSTEM_ID]) { sys_set_mode(mode.mode); // Emit current mode mavlink_msg_sys_status_send(MAVLINK_COMM_0, global_data.state.mav_mode, global_data.state.nav_mode, global_data.state.status, global_data.cpu_usage, global_data.battery_voltage, global_data.motor_block, communication_get_uart_drop_rate()); mavlink_msg_sys_status_send(MAVLINK_COMM_1, global_data.state.mav_mode, global_data.state.nav_mode, global_data.state.status, global_data.cpu_usage, global_data.battery_voltage, global_data.motor_block, communication_get_uart_drop_rate()); } } break; case MAVLINK_MSG_ID_ACTION: { execute_action(mavlink_msg_action_get_action(msg)); //Forwart actions from Xbee to Onboard Computer and vice versa if (chan == MAVLINK_COMM_1) { mavlink_send_uart(MAVLINK_COMM_0, msg); } else if (chan == MAVLINK_COMM_0) { mavlink_send_uart(MAVLINK_COMM_1, msg); } } break; case MAVLINK_MSG_ID_SYSTEM_TIME: { if (!sys_time_clock_get_unix_offset()) { int64_t offset = ((int64_t) mavlink_msg_system_time_get_time_usec( msg)) - (int64_t) sys_time_clock_get_time_usec(); sys_time_clock_set_unix_offset(offset); debug_message_buffer("UNIX offset updated"); } else { // debug_message_buffer("UNIX offset REFUSED"); } } break; case MAVLINK_MSG_ID_REQUEST_DATA_STREAM: { mavlink_request_data_stream_t stream; mavlink_msg_request_data_stream_decode(msg, &stream); switch (stream.req_stream_id) { case 0: // UNIMPLEMENTED break; case 1: // RAW SENSOR DATA global_data.param[PARAM_SEND_SLOT_RAW_IMU] = stream.start_stop; break; case 2: // EXTENDED SYSTEM STATUS global_data.param[PARAM_SEND_SLOT_ATTITUDE] = stream.start_stop; break; case 3: // REMOTE CONTROL CHANNELS global_data.param[PARAM_SEND_SLOT_REMOTE_CONTROL] = stream.start_stop; break; case 4: // RAW CONTROLLER //global_data.param[PARAM_SEND_SLOT_DEBUG_5] = stream.start_stop; //global_data.param[PARAM_SEND_SLOT_DEBUG_3] = stream.start_stop; global_data.param[PARAM_SEND_SLOT_CONTROLLER_OUTPUT] = stream.start_stop; break; case 5: // SENSOR FUSION //LOST IN GROUDNCONTROL // global_data.param[PARAM_SEND_SLOT_DEBUG_5] = stream.start_stop; break; case 6: // POSITION global_data.param[PARAM_SEND_SLOT_DEBUG_5] = stream.start_stop; break; case 7: // EXTRA1 global_data.param[PARAM_SEND_SLOT_DEBUG_2] = stream.start_stop; break; case 8: // EXTRA2 global_data.param[PARAM_SEND_SLOT_DEBUG_4] = stream.start_stop; break; case 9: // EXTRA3 global_data.param[PARAM_SEND_SLOT_DEBUG_6] = stream.start_stop; break; default: // Do nothing break; } } break; case MAVLINK_MSG_ID_PARAM_REQUEST_READ: { mavlink_param_request_read_t set; mavlink_msg_param_request_read_decode(msg, &set); // Check if this message is for this system if ((uint8_t) set.target_system == (uint8_t) global_data.param[PARAM_SYSTEM_ID] && (uint8_t) set.target_component == (uint8_t) global_data.param[PARAM_COMPONENT_ID]) { char* key = (char*) set.param_id; if (set.param_id[0] == '\0') { // Choose parameter based on index if (set.param_index < ONBOARD_PARAM_COUNT) { // Report back value mavlink_msg_param_value_send(chan, (int8_t*) global_data.param_name[set.param_index], global_data.param[set.param_index], ONBOARD_PARAM_COUNT, set.param_index); } } else { for (int i = 0; i < ONBOARD_PARAM_COUNT; i++) { bool match = true; for (int j = 0; j < ONBOARD_PARAM_NAME_LENGTH; j++) { // Compare if (((char) (global_data.param_name[i][j])) != (char) (key[j])) { match = false; } // End matching if null termination is reached if (((char) global_data.param_name[i][j]) == '\0') { break; } } // Check if matched if (match) { // Report back value mavlink_msg_param_value_send(chan, (int8_t*) global_data.param_name[i], global_data.param[i], ONBOARD_PARAM_COUNT, m_parameter_i); } } } } } break; case MAVLINK_MSG_ID_PARAM_REQUEST_LIST: { // Start sending parameters m_parameter_i = 0; } break; case MAVLINK_MSG_ID_PARAM_SET: { mavlink_param_set_t set; mavlink_msg_param_set_decode(msg, &set); // Check if this message is for this system if ((uint8_t) set.target_system == (uint8_t) global_data.param[PARAM_SYSTEM_ID] && (uint8_t) set.target_component == (uint8_t) global_data.param[PARAM_COMPONENT_ID]) { char* key = (char*) set.param_id; for (int i = 0; i < ONBOARD_PARAM_COUNT; i++) { bool match = true; for (int j = 0; j < ONBOARD_PARAM_NAME_LENGTH; j++) { // Compare if (((char) (global_data.param_name[i][j])) != (char) (key[j])) { match = false; } // End matching if null termination is reached if (((char) global_data.param_name[i][j]) == '\0') { break; } } // Check if matched if (match) { // Only write and emit changes if there is actually a difference // AND only write if new value is NOT "not-a-number" // AND is NOT infy if (global_data.param[i] != set.param_value && !isnan(set.param_value) && !isinf(set.param_value)) { global_data.param[i] = set.param_value; // Report back new value mavlink_msg_param_value_send(MAVLINK_COMM_0, (int8_t*) global_data.param_name[i], global_data.param[i], ONBOARD_PARAM_COUNT, m_parameter_i); mavlink_msg_param_value_send(MAVLINK_COMM_1, (int8_t*) global_data.param_name[i], global_data.param[i], ONBOARD_PARAM_COUNT, m_parameter_i); debug_message_buffer_sprintf("Parameter received param id=%i",i); } } } } } break; case MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_SET: { mavlink_position_control_setpoint_set_t pos; mavlink_msg_position_control_setpoint_set_decode(msg, &pos); if (global_data.param[PARAM_POSITIONSETPOINT_ACCEPT] == 1) { // global_data.position_setpoint.x = pos.x; // global_data.position_setpoint.y = pos.y; // global_data.position_setpoint.z = pos.z; debug_message_buffer("Position setpoint updated. OLD?\n"); } else { debug_message_buffer( "Position setpoint recieved but not updated. OLD?\n"); } // Send back a message confirming the new position mavlink_msg_position_control_setpoint_send(MAVLINK_COMM_0, pos.id, pos.x, pos.y, pos.z, pos.yaw); mavlink_msg_position_control_setpoint_send(MAVLINK_COMM_1, pos.id, pos.x, pos.y, pos.z, pos.yaw); } break; case MAVLINK_MSG_ID_POSITION_CONTROL_OFFSET_SET: { mavlink_position_control_offset_set_t set; mavlink_msg_position_control_offset_set_decode(msg, &set); //global_data.attitude_setpoint_pos_body_offset.z = set.yaw; //Ball Tracking if (global_data.param[PARAM_POSITIONSETPOINT_ACCEPT] == 1 && global_data.param[PARAM_POSITION_YAW_TRACKING]==1) { global_data.param[PARAM_POSITION_SETPOINT_YAW] = global_data.attitude.z + set.yaw; mavlink_msg_debug_send(global_data.param[PARAM_SEND_DEBUGCHAN], 92, set.yaw); } } break; case MAVLINK_MSG_ID_SET_CAM_SHUTTER: { // Decode the desired shutter mavlink_set_cam_shutter_t cam; mavlink_msg_set_cam_shutter_decode(msg, &cam); shutter_set(cam.interval, cam.exposure); debug_message_buffer_sprintf("set_cam_shutter. interval %i", cam.interval); } break; case MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL: { uint8_t enable = mavlink_msg_image_trigger_control_get_enable(msg); shutter_control(enable); if (enable) { debug_message_buffer("CAM: Enabling hardware trigger"); } else { debug_message_buffer("CAM: Disabling hardware trigger"); } } break; case MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE: { mavlink_vision_position_estimate_t pos; mavlink_msg_vision_position_estimate_decode(msg, &pos); vision_buffer_handle_data(&pos); // Update validity time is done in vision buffer } break; case MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE: { mavlink_vicon_position_estimate_t pos; mavlink_msg_vicon_position_estimate_decode(msg, &pos); global_data.vicon_data.x = pos.x; global_data.vicon_data.y = pos.y; global_data.vicon_data.z = pos.z; global_data.state.vicon_new_data=1; // Update validity time global_data.vicon_last_valid = sys_time_clock_get_time_usec(); global_data.state.vicon_ok=1; // //Set data from Vicon into vision filter // global_data.vision_data.ang.x = pos.roll; // global_data.vision_data.ang.y = pos.pitch; // global_data.vision_data.ang.z = pos.yaw; // // global_data.vision_data.pos.x = pos.x; // global_data.vision_data.pos.y = pos.y; // global_data.vision_data.pos.z = pos.z; // // global_data.vision_data.new_data = 1; if (!global_data.state.vision_ok) { //Correct YAW global_data.attitude.z = pos.yaw; //If yaw goes to infy (no idea why) set it to setpoint, next time will be better if (global_data.attitude.z > 18.8495559 || global_data.attitude.z < -18.8495559) { global_data.attitude.z = global_data.yaw_pos_setpoint; debug_message_buffer( "vicon CRITICAL FAULT yaw was bigger than 6 PI! prevented crash"); } } //send the vicon message to UART0 with new timestamp mavlink_msg_vicon_position_estimate_send(MAVLINK_COMM_0, global_data.vicon_last_valid, pos.x, pos.y, pos.z, pos.roll, pos.pitch, pos.yaw); } break; case MAVLINK_MSG_ID_PING: { mavlink_ping_t ping; mavlink_msg_ping_decode(msg, &ping); if (ping.target_system == 0 && ping.target_component == 0) { // Respond to ping uint64_t r_timestamp = sys_time_clock_get_unix_time(); mavlink_msg_ping_send(chan, ping.seq, msg->sysid, msg->compid, r_timestamp); } } break; case MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_SET: { mavlink_local_position_setpoint_set_t sp; mavlink_msg_local_position_setpoint_set_decode(msg, &sp); if (sp.target_system == global_data.param[PARAM_SYSTEM_ID]) { if (global_data.param[PARAM_POSITIONSETPOINT_ACCEPT] == 1) { if (sp.x >= global_data.position_setpoint_min.x && sp.y >= global_data.position_setpoint_min.y && sp.z >= global_data.position_setpoint_min.z && sp.x <= global_data.position_setpoint_max.x && sp.y <= global_data.position_setpoint_max.y && sp.z <= global_data.position_setpoint_max.z) { debug_message_buffer("Setpoint accepted and set."); global_data.param[PARAM_POSITION_SETPOINT_X] = sp.x; global_data.param[PARAM_POSITION_SETPOINT_Y] = sp.y; global_data.param[PARAM_POSITION_SETPOINT_Z] = sp.z; if (global_data.param[PARAM_POSITION_YAW_TRACKING] == 0) { // Only update yaw if we are not tracking ball. global_data.param[PARAM_POSITION_SETPOINT_YAW] = sp.yaw; } //check if we want to start or land if (global_data.state.status == MAV_STATE_ACTIVE || global_data.state.status == MAV_STATE_CRITICAL) { if (sp.z > -0.1) { if (!(global_data.state.fly == FLY_GROUNDED || global_data.state.fly == FLY_SINKING || global_data.state.fly == FLY_WAIT_LANDING || global_data.state.fly == FLY_LANDING || global_data.state.fly == FLY_RAMP_DOWN)) { //if setpoint is lower that ground iate landing global_data.state.fly = FLY_SINKING; global_data.param[PARAM_POSITION_SETPOINT_Z] = -0.2;//with lowpass debug_message_buffer( "Sinking for LANDING. (z-sp lower than 10cm)"); } else if (!(global_data.state.fly == FLY_GROUNDED)) { global_data.param[PARAM_POSITION_SETPOINT_Z] = -0.2;//with lowpass } } else if (global_data.state.fly == FLY_GROUNDED && sp.z < -0.50) { //start if we were grounded and get a sp over 0.5m global_data.state.fly = FLY_WAIT_MOTORS; debug_message_buffer( "STARTING wait motors. (z-sp higher than 50cm)"); //set point changed with lowpass, after 5s it will be ok. } } //SINK TO 0.7m if we are critical or emergency if (global_data.state.status == MAV_STATE_EMERGENCY || global_data.state.status == MAV_STATE_CRITICAL) { global_data.param[PARAM_POSITION_SETPOINT_Z] = -0.7;//with lowpass } } else { debug_message_buffer("Setpoint refused. Out of range."); } } else { debug_message_buffer("Setpoint refused. Param setpoint accept=0."); } } } break; default: break; } }
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 */ warnx("terminating..."); 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 = hrt_absolute_time(); 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.x = pos.x; vicon_position.y = pos.y; vicon_position.z = pos.z; 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); } } //Mavlink Message from the onboard computer / laserscanner: if (msg->msgid == MAVLINK_MSG_ID_DANGER) { mavlink_danger_t dang; mavlink_msg_danger_decode(msg, &dang); struct danger_s d; d.time_usec = hrt_absolute_time(); d.sensor_id = dang.sensor_id; d.danger_level = dang.danger_level; d.danger_dist = dang.danger_dist; d.danger_dir = dang.danger_dir; d.avoid_level = dang.avoid_level; d.avoid_dir = dang.avoid_dir; //check if topic is advertised if (danger_pub <= 0) { danger_pub = orb_advertise(ORB_ID(danger), &d); } else { // publish orb_publish(ORB_ID(danger), danger_pub, &d); } } /* 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); } } } }
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); } } } }
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); } } } }