Integrator.STMCalculationMethod Property

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Description

A flag indicating the method to be used to calculate the state transition matrix. Note that even if the CalculateSTM property is set to FALSE, this property still applies if the SpacecraftODProperties.PropagateCovariance flag is to TRUE or if the Spacecraft is included in an estimation process.

 

Timing Precision Mode

This page describes functionality 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 = myIntegrator1.STMCalculationMethod;

 

myIntegrator1.STMCalculationMethod = myVariable1;

 

See also

Integrator Object

Spacecraft Propagators

Setting up an Integrator