|
| | (0x80,0x01) Raw Accel |
| | Three element vector representing the sensed acceleration. This quantity is temperature compensated and expressed in the sensor body frame.
|
| |
| | (0x80,0x02) Raw Gyro |
| | Three element vector representing the sensed angular rate. This quantity is temperature compensated and expressed in the sensor body frame.
|
| |
| | (0x80,0x03) Raw Mag |
| | Three element vector representing the sensed magnetic field. This quantity is temperature compensated and expressed in the vehicle frame.
|
| |
| | (0x80,0x16) Raw Pressure |
| | Scalar value representing the sensed ambient pressure. This quantity is temperature compensated.
|
| |
| | (0x80,0x04) Scaled Accel |
| | 3-element vector representing the sensed acceleration. This quantity is temperature compensated and expressed in the vehicle frame.
|
| |
| | (0x80,0x05) Scaled Gyro |
| | 3-element vector representing the sensed angular rate. This quantity is temperature compensated and expressed in the vehicle frame.
|
| |
| | (0x80,0x06) Scaled Mag |
| | 3-element vector representing the sensed magnetic field. This quantity is temperature compensated and expressed in the vehicle frame.
|
| |
| | (0x80,0x17) Scaled Pressure |
| | Scalar value representing the sensed ambient pressure.
|
| |
| | (0x80,0x07) Delta Theta |
| | 3-element vector representing the time integral of angular rate. This quantity is the integral of sensed angular rate over the period set by the IMU message format. It is expressed in the vehicle frame.
|
| |
| | (0x80,0x08) Delta Velocity |
| | 3-element vector representing the time integral of acceleration. This quantity is the integral of sensed acceleration over the period set by the IMU message format. It is expressed in the vehicle frame.
|
| |
| | (0x80,0x09) Comp Orientation Matrix |
| | 3x3 Direction Cosine Matrix EQSTART M_{ned}^{veh} EQEND describing the orientation of the device with respect to the NED local-level frame. This matrix satisfies the following relationship:
|
| |
| | (0x80,0x0A) Comp Quaternion |
| | 4x1 vector representation of the quaternion describing the orientation of the device with respect to the NED local-level frame. This quaternion satisfies the following relationship:
|
| |
| | (0x80,0x0C) Comp Euler Angles |
| | Euler angles describing the orientation of the device with respect to the NED local-level frame. The Euler angles are reported in 3-2-1 (Yaw-Pitch-Roll, AKA Aircraft) order.
|
| |
| | (0x80,0x0B) Comp Orientation Update Matrix |
| | DEPRECATED!
|
| |
| | (0x80,0x0D) Orientation Raw Temp |
| | DEPRECATED!
|
| |
| | (0x80,0x0E) Internal Timestamp |
| | DEPRECATED!
|
| |
| | (0x80,0x0F) Pps Timestamp |
| | DEPRECATED!
|
| |
| | (0x80,0x12) Gps Timestamp |
| | GPS timestamp of the SENSOR data.
|
| |
| | (0x80,0x14) Temperature Abs |
| | SENSOR reported temperature statistics.
|
| |
| | (0x80,0x11) Up Vector |
| | Gyro-stabilized 3-element vector representing the complementary filter's estimated vertical direction. This quantity is expressed in the vehicle frame.
|
| |
| | (0x80,0x10) North Vector |
| | Gyro-stabilized 3-element vector representing the complementary filter's estimate of magnetic north. This quantity is expressed in the vehicle frame.
|
| |
| | (0x80,0x18) Overrange Status |
| |
| | (0x80,0x40) Odometer Data |
| |
