Description
Properties for the Time Varying attitude control for a Finite Maneuver.
Public Properties
 Az0 | Azimuth constant term (dimension: angle). |
| Az1 | Azimuth linear term (dimension: angle/time). |
| Az2 | Azimuth quadratic term (dimension: angle/time^2). |
| Az3 | Azimuth cubic term (dimension: angle/time^3). |
| Az4 | Azimuth quartic term (dimension: angle/time^4). |
| AzA | Azimuth sine term amplitude (dimension: angle). |
| AzF | Azimuth sine term frequency (dimension: angle/time). |
| AzP | Azimuth sine term phase (dimension: angle). |
| BodyConstraintVector | Defines a constraint vector in spacecraft body coordinates to complete the attitude definition. |
| El0 | Elevation constant term (dimension: angle). |
| El1 | Elevation linear term (dimension: angle/time). |
| El2 | Elevation quadratic term (dimension: angle/time^2). |
| El3 | Elevation cubic term (dimension: angle/time^3). |
| El4 | Elevation quartic term (dimension: angle/time^4). |
| ElA | Elevation sine term amplitude (dimension: angle). |
| ElF | Elevation sine term frequency (dimension: angle/time). |
| ElP | Elevation sine term phase (dimension: angle). |
| ThrustAxesName | Gets or sets the thrust axes. |
Interfaces
| Implemented Interface |
|---|
| IAgVAAttitudeControl |
| IAgVAAttitudeControlFinite |