Description
Populates the Formation with states 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 Spacecrafts' 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
Arguments
meanState
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Description:
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The mean state associated with the covariance matrix. The returned states are 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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random
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Description:
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RandomNumberGenerator object to use when computing random states.
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Syntax
myFormation1.SetRandomStates(myArray1, myMatrix1, myString1, myRandomNumberGenerator1);
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See also
Formation Object
Formation.SetRandomStates
Formations Guide
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