Description
Attitude Control options.
Members
| Member | Value | Description |
|---|---|---|
| eVAAttitudeControlVelocityVector | 0 | Along Velocity Vector (impulsive/finite) - the total thrust vector is aligned with the spacecraft's velocity vector. |
| eVAAttitudeControlAntiVelocityVector | 1 | Anti-Velocity Vector (impulsive/finite) - the total thrust vector is opposite to the spacecraft's velocity vector. |
| eVAAttitudeControlAttitude | 2 | Attitude (impulsive/finite) - the thrust vector direction is defined using Euler Angles or a Quaternion. |
| eVAAttitudeControlFile | 3 | File (impulsive/finite) - uses an attitude file to set the thrust vector direction. |
| eVAAttitudeControlThrustVector | 4 | Thrust Vector (impulsive/finite) - the total thrust vector is explicitly specified in Cartesian or spherical form with respect to the thrust axes. |
| eVAAttitudeControlPlugin | 5 | Plugin (finite) - thrust vector direction is defined using a COM plugin. |
| eVAAttitudeControlTimeVarying | 6 | Time Varying (finite) - polynomial and sine representations for the azimuth and elevation of the thrust vector. |
| eVAAttitudeControlLagrangeInterpolation | 7 | Lagrange Interpolation (optimal finite, always set) - supports the 'Run current nodes' execution mode of the Optimal Finite Maneuver. |