The components of the thrust vector in the coordinates of the attitude system specified by the chosen AttitudeSystem.
For each attitude system the maneuver components are defined as follows:
In the above descriptions, the Orbit Normal is aligned with the angular momentum vector, the Negative Orbit Normal is aligned with the negative angular momentum vector, and Nadir points to the center of the Earth. The X-components of the VNB and LVLH coordinate systems, Velocity and Co-Velocity, differ by a rotation about the flight path angle. For more information on each of the coordinate systems above, see the Attitude Reference Frames page.
Timing Precision Mode
This page describes functionality in millisecond timing precision mode.
Click here to see the documentation for this object in nanosecond timing precision mode.