AttitudeControl#
- class ansys.stk.core.stkobjects.astrogator.AttitudeControl#
IntEnum
Overview#
|
Along Velocity Vector (impulsive/finite) - the total thrust vector is aligned with the spacecraftβs velocity vector. |
|
Anti-Velocity Vector (impulsive/finite) - the total thrust vector is opposite to the spacecraftβs velocity vector. |
|
Attitude (impulsive/finite) - the thrust vector direction is defined using Euler Angles or a Quaternion. |
|
File (impulsive/finite) - uses an attitude file to set the thrust vector direction. |
|
Thrust Vector (impulsive/finite) - the total thrust vector is explicitly specified in Cartesian or spherical form with respect to the thrust axes. |
|
Plugin (finite) - thrust vector direction is defined using a COM plugin. |
|
Time Varying (finite) - polynomial and sine representations for the azimuth and elevation of the thrust vector. |
|
Lagrange Interpolation (optimal finite, always set) - supports the βRun current nodesβ execution mode of the Optimal Finite Maneuver. |
Import detail#
from ansys.stk.core.stkobjects.astrogator import AttitudeControl