Description
Attitude Control options.
Members
| Member | Value | Description |
|---|---|---|
| eVAAttitudeControlVelocityVector | 0 | Along Velocity Vector - attitude is such that the total thrust vector is aligned with the spacecraft's inertial velocity vector. |
| eVAAttitudeControlAntiVelocityVector | 1 | Anti-Velocity Vector - attitude is such that the total thrust vector is opposite to the spacecraft's inertial velocity vector. |
| eVAAttitudeControlAttitude | 2 | Attitude - attitude is defined using Euler Angles or a Quaternion. |
| eVAAttitudeControlFile | 3 | File - import an attitude file to set the maneuver. |
| eVAAttitudeControlThrustVector | 4 | Thrust Vector - the total thrust vector can be specified in cartesian or spherical form with respect to the thrust axes. |
| eVAAttitudeControlPlugin | 5 | Plugin - attitude is defined using a COM plugin. |
| eVAAttitudeControlTimeVarying | 6 | Time Varying - polynomial and sine representations for the azimuth and elevation of the thrust vector. |