Spacecraft.GetElementSetToElementSetJacobian(String, String) Method

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Description

Returns the Jacobian that maps from one element set to another.

 

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

Spacecraft.GetElementSetToElementSetJacobian(

String elementSetFromWhichToMap,


String elementSetToWhichToMap)

 

 

Arguments

elementSetFromWhichToMap


Description:

The element set from which the mapping will be done (this is the set in the denominator of the Jacobian partials).

Valid Values:

Value

Label

"Cartesian"

Cartesian

"Equinoctial"

Equinoctial

"SGP4Equinoctial"

SGP4Equinoctial

"NoradEquinoctial"

NoradEquinoctial (deprecated, use SGP4Equinoctial instead)

 

 

 

elementSetToWhichToMap


Description:

The element set to which the mapping will be done (this is the set in the numerator of the Jacobian partials).

Valid Values:

Value

Label

"Cartesian"

Cartesian

"Equinoctial"

Equinoctial

 

 

 

 

Return Value

Type:

Matrix of number (size = 6 x 6)

 

 

The value of the specified Covariance matrix element.

 

Syntax

myMatrix1 = mySpacecraft1.GetElementSetToElementSetJacobian(myString1, myString2);

 

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide