Styles by Object | Missile Report Styles | Missile Graph Styles
Report Style: Attitude Quaternions
The attitude quaternion of the vehicle's body axes computed with respect to the vehicle's central body inertial coordinate system. The quaternion components q1, q2, and q3 are the vector components of the quaternion; q4 is the scalar part.Data Provider:Attitude Quaternions
Type: Time-varying data.
Availability: Reports | Dynamic Displays
Column Listing
Column | Column Name | Element | Type | Dimension | Description |
---|---|---|---|---|---|
1 | Time | Time | Real Number or Text | Date | Time. |
2 | q1 | q1 | Real Number | Unitless | First element of quaternion (and of its vector part) representing the orientation between the body and Inertial axes. |
3 | q2 | q2 | Real Number | Unitless | Second element of quaternion (and of its vector part) representing the orientation between the body and Inertial axes. |
4 | q3 | q3 | Real Number | Unitless | Third element of quaternion (and of its vector part) representing the orientation between the body and Inertial axes. |
5 | q4 | q4 | Real Number | Unitless | Fourth element of quaternion (its scalar part) representing the orientation between the body and Inertial axes. |