Description
Populates the Spacecraft state using a random state from a Gaussian distribution described by the provided covariance matrix. The dimension and order of the covariance matrix is assumed to be consistent with the Spacecraft's ProcessAction settings.
Timing Precision Mode
This page describes functionality in nanosecond timing precision mode.
Click here to see the documentation for this object in millisecond timing precision mode.
Method Signature
Spacecraft.SetRandomState(
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Array meanState,
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Matrix covariance,
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String covarianceElementSet)
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Arguments
meanState
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Description:
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The mean state associated with the covariance matrix. The returned states is referenced from the provided mean.
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covariance
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Description:
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The covariance matrix that describes the Gaussian distribution from which to draw a state.
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covarianceElementSet
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Description:
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Element set definition of the provided covariance.
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Valid Values:
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Value
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Label
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"Cartesian"
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Cartesian Elements
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"Equinoctial"
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Equinoctial Elements
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"SGP4Equinoctial"
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SGP4Equinoctial Elements
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"NoradEquinoctial"
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NoradEquinoctial Elements (deprecated, use SGP4Equinoctial instead)
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Syntax
mySpacecraft1.SetRandomState(myArray1, myMatrix1, myString1);
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See also
Spacecraft Object
Spacecraft.SetRandomState
Spacecraft Propagation Guide
Coverage and Contact Analysis Guide
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