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Copy file name to clipboardExpand all lines: ko/messages/common.md
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@@ -2156,7 +2156,7 @@ The position must be set automatically by the system during the takeoff, and may
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The global and local positions encode the position in the respective coordinate frames, while the q parameter encodes the orientation of the surface.
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Under normal conditions it describes the heading and terrain slope, which can be used by the aircraft to adjust the approach.
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The approach 3D vector describes the point to which the system should fly in normal flight mode and then perform a landing sequence along the vector.
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Note: this message can be requested by sending the [MAV_CMD_REQUEST_MESSAGE](#MAV_CMD_REQUEST_MESSAGE) with param1=242 (or the deprecated [MAV_CMD_GET_HOME_POSITION](#MAV_CMD_GET_HOME_POSITION) command).
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Note: this message can be requested by sending the [MAV_CMD_REQUEST_MESSAGE](#MAV_CMD_REQUEST_MESSAGE) with param1=242.
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The interval between messages for a particular MAVLink message ID.
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This message is sent in response to the [MAV_CMD_REQUEST_MESSAGE](#MAV_CMD_REQUEST_MESSAGE) command with param1=244 (this message) and param2=message_id (the id of the message for which the interval is required).
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It may also be sent in response to [MAV_CMD_GET_MESSAGE_INTERVAL](#MAV_CMD_GET_MESSAGE_INTERVAL).
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This interface replaces [DATA_STREAM](#DATA_STREAM).
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| Field Name | Type | Units | Description |
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### UAVCAN_NODE_INFO (311) {#UAVCAN_NODE_INFO}
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General information describing a particular UAVCAN node. Please refer to the definition of the UAVCAN service "uavcan.protocol.GetNodeInfo" for the background information. This message should be emitted by the system whenever a new node appears online, or an existing node reboots. Additionally, it can be emitted upon request from the other end of the MAVLink channel (see [MAV_CMD_UAVCAN_GET_NODE_INFO](#MAV_CMD_UAVCAN_GET_NODE_INFO)). It is also not prohibited to emit this message unconditionally at a low frequency. The UAVCAN specification is available at http://uavcan.org.
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General information describing a particular UAVCAN node.
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Please refer to the definition of the UAVCAN service "uavcan.protocol.GetNodeInfo" for the background information.
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This message should be emitted by the system whenever a new node appears online, or an existing node reboots.
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The message may also be explicitly requested using [MAV_CMD_REQUEST_MESSAGE](#MAV_CMD_REQUEST_MESSAGE).
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It is also not prohibited to emit this message unconditionally at a low frequency.
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The DroneCAN specification is available at https://dronecan.github.io/Specification/1._Introduction/.
| <a id='GLOBAL_POSITION_SRC_UNKNOWN'></a>0 | [GLOBAL_POSITION_SRC_UNKNOWN](#GLOBAL_POSITION_SRC_UNKNOWN) | Source is unknown or not one of the listed types. |
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| <a id='GLOBAL_POSITION_SRC_GNSS'></a>1 | [GLOBAL_POSITION_SRC_GNSS](#GLOBAL_POSITION_SRC_GNSS) | Global Navigation Satellite System (e.g.: GPS, Galileo, Glonass, BeiDou). |
| <a id='GLOBAL_POSITION_SRC_PSEUDOLITES'></a>3 | [GLOBAL_POSITION_SRC_PSEUDOLITES](#GLOBAL_POSITION_SRC_PSEUDOLITES) | A pseudo-satellite system using transceiver beacons to perform GNSS-like positioning. |
| <a id='GLOBAL_POSITION_SRC_MAGNETIC'></a>5 | [GLOBAL_POSITION_SRC_MAGNETIC](#GLOBAL_POSITION_SRC_MAGNETIC) | Magnetic positioning. |
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| <a id='GLOBAL_POSITION_SRC_ESTIMATOR'></a>6 | [GLOBAL_POSITION_SRC_ESTIMATOR](#GLOBAL_POSITION_SRC_ESTIMATOR) | Estimated position based on various sensors (eg. a Kalman Filter). |
| <a id='GLOBAL_POSITION_SRC_UNKNOWN'></a>0 | [GLOBAL_POSITION_SRC_UNKNOWN](#GLOBAL_POSITION_SRC_UNKNOWN) | Source is unknown or not one of the listed types. |
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| <a id='GLOBAL_POSITION_SRC_GNSS'></a>1 | [GLOBAL_POSITION_SRC_GNSS](#GLOBAL_POSITION_SRC_GNSS) | Global Navigation Satellite System (e.g.: GPS, Galileo, Glonass, BeiDou). |
| <a id='GLOBAL_POSITION_SRC_PSEUDOLITES'></a>3 | [GLOBAL_POSITION_SRC_PSEUDOLITES](#GLOBAL_POSITION_SRC_PSEUDOLITES) | A pseudo-satellite system using transceiver beacons to perform GNSS-like positioning. |
| <a id='GLOBAL_POSITION_SRC_MAGNETIC'></a>5 | [GLOBAL_POSITION_SRC_MAGNETIC](#GLOBAL_POSITION_SRC_MAGNETIC) | Magnetic positioning. |
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| <a id='GLOBAL_POSITION_SRC_ESTIMATOR'></a>6 | [GLOBAL_POSITION_SRC_ESTIMATOR](#GLOBAL_POSITION_SRC_ESTIMATOR) | Estimated position based on various sensors (eg. a Kalman Filter). |
<span class="warning">**SUPERSEDED:** Replaced By [MAV_CMD_REQUEST_MESSAGE](#MAV_CMD_REQUEST_MESSAGE) (2026-05)</span>
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Commands the vehicle to respond with a sequence of messages [UAVCAN_NODE_INFO](#UAVCAN_NODE_INFO), one message per every UAVCAN node that is online. Note that some of the response messages can be lost, which the receiver can detect easily by checking whether every received [UAVCAN_NODE_STATUS](#UAVCAN_NODE_STATUS) has a matching message [UAVCAN_NODE_INFO](#UAVCAN_NODE_INFO) received earlier; if not, this command should be sent again in order to request re-transmission of the node information messages.
| <aid='ACTUATOR_TEST_GROUP_ROLL_TORQUE'></a>0 |[ACTUATOR_TEST_GROUP_ROLL_TORQUE](#ACTUATOR_TEST_GROUP_ROLL_TORQUE)| Actuators that contribute to roll torque. |
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| <aid='ACTUATOR_TEST_GROUP_PITCH_TORQUE'></a>1 |[ACTUATOR_TEST_GROUP_PITCH_TORQUE](#ACTUATOR_TEST_GROUP_PITCH_TORQUE)| Actuators that contribute to pitch torque. |
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| <aid='ACTUATOR_TEST_GROUP_YAW_TORQUE'></a>2 |[ACTUATOR_TEST_GROUP_YAW_TORQUE](#ACTUATOR_TEST_GROUP_YAW_TORQUE)| Actuators that contribute to yaw torque. |
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| <aid='ACTUATOR_TEST_GROUP_COLLECTIVE_TILT'></a>3 |[ACTUATOR_TEST_GROUP_COLLECTIVE_TILT](#ACTUATOR_TEST_GROUP_COLLECTIVE_TILT)| Actuators that affect collective tilt. |
| <aid='ACTUATOR_TEST_GROUP_ROLL_TORQUE'></a>0 |[ACTUATOR_TEST_GROUP_ROLL_TORQUE](#ACTUATOR_TEST_GROUP_ROLL_TORQUE)| Actuators that contribute to roll torque. |
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| <aid='ACTUATOR_TEST_GROUP_PITCH_TORQUE'></a>1 |[ACTUATOR_TEST_GROUP_PITCH_TORQUE](#ACTUATOR_TEST_GROUP_PITCH_TORQUE)| Actuators that contribute to pitch torque. |
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| <aid='ACTUATOR_TEST_GROUP_YAW_TORQUE'></a>2 |[ACTUATOR_TEST_GROUP_YAW_TORQUE](#ACTUATOR_TEST_GROUP_YAW_TORQUE)| Actuators that contribute to yaw torque. |
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| <aid='ACTUATOR_TEST_GROUP_COLLECTIVE_TILT'></a>3 |[ACTUATOR_TEST_GROUP_COLLECTIVE_TILT](#ACTUATOR_TEST_GROUP_COLLECTIVE_TILT)| Actuators that affect collective tilt. |
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| <aid='ACTUATOR_TEST_GROUP_X_THRUST'></a>4 |[ACTUATOR_TEST_GROUP_X_THRUST](#ACTUATOR_TEST_GROUP_X_THRUST)| Actuators that contribute to x (longitudinal, positive = forward) thrust. |
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| <aid='ACTUATOR_TEST_GROUP_Y_THRUST'></a>5 |[ACTUATOR_TEST_GROUP_Y_THRUST](#ACTUATOR_TEST_GROUP_Y_THRUST)| Actuators that contribute to y (lateral, positive = right) thrust. |
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| <aid='ACTUATOR_TEST_GROUP_Z_THRUST'></a>6 |[ACTUATOR_TEST_GROUP_Z_THRUST](#ACTUATOR_TEST_GROUP_Z_THRUST)| Actuators that contribute to z (vertical, positive = down) thrust. |
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