Satellite: Attitude Segment YPR

The attitude of the vehicle with respect to the vehicle's central body inertial coordinate system, expressed using YPR angles. Additionally, provides information on the attitude segment being used at the given time. YPR angles specify attitude using three rotations in sequence: a rotation about the X axis is called roll (R), a rotation about the Y axis is called pitch (P), and a rotation about the Z axis is called yaw (Y). 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.

Type: Time-varying data. Intended to be used only with elements from this same data provider.

Availability: Reports | Graphs | Dynamic Displays | Strip Charts

Name Description
Seq RPY Attitude represented using the sequence of rotations about the X axis, then about the Y axis, then about the Z axis.
Seq RYP Attitude represented using the sequence of rotations about the X axis, then about the Z axis, then about the Y axis.
Seq PRY Attitude represented using the sequence of rotations about the Y axis, then about the X axis, then about the Z axis.
Seq PYR Attitude represented using the sequence of rotations about the Y axis, then about the Z axis, then about the X axis.
Seq YRP Attitude represented using the sequence of rotations about the Z axis, then about the X axis, then about the Y axis.
Seq YPR Attitude represented using the sequence of rotations about the Z axis, then about the Y axis, then about the X axis.

STK Programming Interface 11.0.1