Styles by Object | LaunchVehicle Report Styles | LaunchVehicle Graph Styles
Report Style: Yaw Pitch Roll
The attitude of the vehicle (i.e., the rotation between the vehicle's body axes and the vehicle' central body's inertial frame), expressed using 321 YPR angles, as a function of time. YPR angles use a sequence of three rotations starting from a reference coordinate frame. Unlike Euler angles, the rotations are not made about axes defined by an earlier rotation: each rotation is made about the reference system's axes. The 321 sequence uses Z, then Y, and then finally the X axis.As used in YPR angles, the names yaw, pitch, and roll do not refer to the angles normally used in aviation; the terms yaw, pitch, and roll in aviation refer to 321 Euler angles.
Data Provider:Attitude YPR
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 | Yaw | Yaw | Real Number or Text | Angle | Yaw angle, i.e., the rotation angle about the reference Z-axis. |
3 | Pitch | Pitch | Real Number or Text | Angle | Pitch angle, i.e., the rotation angle about the reference Y-axis. |
4 | Roll | Roll | Real Number or Text | Angle | Roll angle, i.e., the rotation angle about the reference X-axis. |