SpacecraftODProperties.CovariancePropagationMethod Property

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Description

This property has been Deprecated. Please use (Spacecraft.Propagator AsType Integrator).STMCalculationMethod instead.

A flag indicating the method to be used to calculate the State Transition Matrix to propagate the Covariance.

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.

Attributes

Type:

integer

Access:

read/write

Default Value:

2 ( Variational Equations )

Valid Values:

Value	Label
0	J2 Semi-Analytic
1	Numeric
2	Variational Equations

Syntax

myVariable1 = mySpacecraftODProperties1.CovariancePropagationMethod;

mySpacecraftODProperties1.CovariancePropagationMethod = myVariable1;