Covariance6By6TwoBodyBlender Properties |
The Covariance6By6TwoBodyBlender type exposes the following members.
Properties| Name | Description | |
|---|---|---|
 | CovarianceAxes |
Gets or sets the native axes of the CovarianceData.
|
| CovarianceData |
Gets or sets the covariance data that is used for blending.
|
| DateTolerance |
Gets or sets the tolerance in seconds that is used to ensure that the dates in OrbitStates
and CovarianceData are close enough to being equal. By default, this value is
Epsilon6.
|
| GravitationalParameter |
Gets or sets the gravitational parameter of the central body that the spacecraft is orbiting.
|
| InertialPropagationFrame |
Gets or sets the inertial propagation frame that is used to propagate the OrbitStates
and the CovarianceData.
|
| IsFrozen |
Gets a value indicating whether this object is frozen. A frozen object cannot be modified and an
ObjectFrozenException will be thrown if an attempt is made to do so.
(Inherited from DefinitionalObject.) |
| OrbitStates |
Gets or sets the position and velocity vectors of the spacecraft at the same times
as the CovarianceData.
|
| OrbitStatesFrame |
Gets or sets the native reference frame of the OrbitStates.
|
See Also