Spacecraft.VehicleDryMOI Property

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Description

The dry vehicle moment of inertia matrix (i.e. no attached Tanks are included in this property). This property is used in calculating the Spacecraft MomentOfInertia, which includes all attached Tanks in its calculation. The MOI is referenced from the origin of the Spacecraft BCS.

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

 

Attributes

Type:

Matrix of number (size = 3 x 3)

Access:

read/write

Units:

kg m2

Default Value:

[1200,0,0;0,1200,0;0,0,1200]

 

Syntax

myMatrix1 = mySpacecraft1.VehicleDryMOI;

 

mySpacecraft1.VehicleDryMOI = myMatrix1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide