Data Provider Groups | Data Provider Elements

Attitude YPR

The attitude of the vehicle with respect to the vehicle's central body inertial coordinate system, expressed using YPR angles.

Similar to Euler angles, YPR angles specify attitude using three rotations in sequence: a rotation about the reference X axis is called roll (R), a rotation about the reference Y axis is called pitch (P), and a rotation about the reference 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.

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.



Available for these objects: LaunchVehicle, Missile, Satellite

Type: Time-varying data.

Availability: Reports | Graphs | Dynamic Displays | Strip Charts

Data Provider Groups

NameDescription
Seq RPYAttitude represented using the sequence of rotations about the X axis, then about the Y axis, then about the Z axis.
Seq RYPAttitude represented using the sequence of rotations about the X axis, then about the Z axis, then about the Y axis.
Seq PRYAttitude represented using the sequence of rotations about the Y axis, then about the X axis, then about the Z axis.
Seq PYRAttitude represented using the sequence of rotations about the Y axis, then about the Z axis, then about the X axis.
Seq YRPAttitude represented using the sequence of rotations about the Z axis, then about the X axis, then about the Y axis.
Seq YPRAttitude represented using the sequence of rotations about the Z axis, then about the Y axis, then about the X axis.

Data Provider Elements

NameDimensionTypeDescription
TimeDateReal Number or TextTime.
YawAngleReal Number or TextYaw angle, i.e., the rotation angle about the reference Z-axis.
PitchAngleReal Number or TextPitch angle, i.e., the rotation angle about the reference Y-axis.
RollAngleReal Number or TextRoll angle, i.e., the rotation angle about the reference X-axis.
Yaw RateAngleRateReal NumberThe rate of change of yaw angle.
Pitch RateAngleRateReal NumberThe rate of change of pitch angle.
Roll RateAngleRateReal NumberThe rate of change of roll angle.