Spacecraft.EPV(AcqData) Method

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Description

Extended Precision Vectors give spacecraft position and velocity information in the Geocentric True of Date Rotating reference frame.

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

 

Note: This is an interval method. See the Interval Methods page for more information.

Note: This method has a state. See the Methods and Properties with State page for more information.

 

Method Signature

Spacecraft.EPV(

AcqData dataConfiguration)

 

Arguments

dataConfiguration


Description:

AcqData object that contains all the configuration information used to generate the EPV report.

 

 

Return Value

Type:

string

 

Returns spacecraft position and velocity information in the Geocentric True of Date Rotating reference frame.

 

Syntax

myString1 = mySpacecraft1.EPV(myAcqData1);

 

Example 1

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide