Spacecraft.SimulateTrackingData(EquinoctialStateObservation) Method

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Description

This method simulates Equinoctial State Observation data.

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.SimulateTrackingData(

EquinoctialStateObservation eqObservation)

Arguments

eqObservation
Description:	The Equinoctial State Observation to be populated with simulated data.

Return Value

Type:

number

Returns 1 if data was successfully simulated, 0 if no data was simulated due to a visibility restriction, such as an occulting body or sensor mask. When simulating multiple Pseudorange Observations, this method returns the number simulated.

Syntax

myVariable1 = mySpacecraft1.SimulateTrackingData(myEquinoctialStateObservation1);