ThrustEvent.AttitudeSystem Property

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Description

Flag denoting the attitude frame in which the thrust event will be applied to the spacecraft.

 

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.

 

Attributes

Type:

integer

Access:

read/write

Default Value:

0 ( Mean of J2000 )

Valid Values:

Value

Label

0

Mean of J2000

1

VNB

2

LVLH

3

Body Fixed

4

GEODETIC

5

UVW

6

RIC

 

Syntax

myVariable1 = myThrustEvent1.AttitudeSystem;

 

myThrustEvent1.AttitudeSystem = myVariable1;

 

See also

ThrustEvent Object