CovarianceUtilities.CalculateMeanAndCovariance(Formation, Array) Method

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Description

Calculates and returns the covariance of a distribution of orbit states defined in the Spacecraft in the provided Formation. Also, populates the meanState argument with the computed mean state.

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

Method Signature

CovarianceUtilities.CalculateMeanAndCovariance(	Formation formation,
	Array meanState)

Arguments

formation
Description:	Formation object containing the states to use when computing the covariance.

meanState
Description:	The computed mean state associated with the covariance matrix.

Return Value

Type:

Matrix of number

Returns a covariance matrix.

Syntax

myMatrix1 = CovarianceUtilities.CalculateMeanAndCovariance(myFormation1, myArray1);