Spacecraft.EulerAnglesMJ2000 Property

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Description

This property has been Deprecated. Please use Spacecraft.EulerAnglesICRF instead. This property returns values referenced from the system inertial frame rather than the MJ2000 Earth Equator frame.

 

Returns the three Euler Angles that define the orientation of the Spacecraft Body Coordinate System with respect to the ICRF. 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 nanosecond timing precision mode.

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

 

Attributes

Type:

Array of number (size = 3)

Access:

read

Units:

deg

 

Syntax

myVariable1 = mySpacecraft1.EulerAnglesMJ2000[0];

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide