Spacecraft.AttitudeMJ2000 Property

Top 

Description

This property has been Deprecated. Please use Spacecraft.EulerAnglesMJ2000 instead.

 

Returns the three Euler Angles that define the orientation of the Spacecraft Body Coordinate System with respect to the Mean of J2000 Earth-Equator coordinate frame. This property does not affect the Euler Angle Sequence. Please use Spacecraft.EulerSequence to set the Euler Angle rotation sequence.

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode.

 

Attributes

Type:

Array of number (size = 3)

Access:

read

Units:

deg

 

Syntax

myVariable1 = mySpacecraft1.AttitudeMJ2000[0];

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide