RotatingPulsatingSystem.ReferenceVector Property

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Description

The second vector used in establishing the frame. For a closed, bounded orbit (such as Earth-Moon), this should be the velocity vector of the Secondary Object. For alternately retro- and prograde motion (such as Earth-Mars), this should be a nearly constant vector, such as MJ2K Earth Ecliptic North.

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

 

Attributes

Type:

integer

Access:

read/write

Default Value:

0 ( Relative Velocity at the Instantaneous Time )

Valid Values:

Value

Label

0

Relative Velocity at the Instantaneous Time

1

MJ2K Earth Equator North

2

MJ2K Earth Ecliptic North

 

Syntax

myVariable1 = myRotatingPulsatingSystem1.ReferenceVector;

 

myRotatingPulsatingSystem1.ReferenceVector = myVariable1;

 

See also

RotatingPulsatingSystem Object

Rotating-Pulsating Systems Guide