EquinoctialStateObservation(Spacecraft) Constructor

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Description

Create a EquinoctialStateObservation object, and associate it with the "objectBeingMeasured".

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

 

Constructor Signature

EquinoctialStateObservation(

Spacecraft objectBeingEstimated)

 

 

Arguments

objectBeingEstimated

Description:

The spacecraft whose state state is being fit to the target / reference state.

 

 

 

Syntax

EquinoctialStateObservation myEquinoctialStateObservation1(mySpacecraft1);

 

 

See also

EquinoctialStateObservation Object