Description
Returns the Jacobian that maps from one element set to another.
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
Spacecraft.GetElementSetToElementSetJacobian(
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String elementSetFromWhichToMap,
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String elementSetToWhichToMap)
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Arguments
elementSetFromWhichToMap
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Description:
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The element set from which the mapping will be done (this is the set in the denominator of the Jacobian partials).
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Valid Values:
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Value
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Label
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"Cartesian"
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Cartesian
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"Equinoctial"
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Equinoctial
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"SGP4Equinoctial"
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SGP4Equinoctial
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"NoradEquinoctial"
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NoradEquinoctial (deprecated, use SGP4Equinoctial instead)
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elementSetToWhichToMap
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Description:
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The element set to which the mapping will be done (this is the set in the numerator of the Jacobian partials).
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Valid Values:
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Value
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Label
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"Cartesian"
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Cartesian
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"Equinoctial"
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Equinoctial
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Return Value
Type:
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Matrix of number (size = 6 x 6)
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The value of the specified Covariance matrix element.
Syntax
myMatrix1 = mySpacecraft1.GetElementSetToElementSetJacobian(myString1, myString2);
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See also
Spacecraft Object
Spacecraft Propagation Guide
Coverage and Contact Analysis Guide
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