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 nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond 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;

 

See also

SpacecraftODProperties Object

Orbit Determination Guide