Spacecraft.VehicleDryCenterOfGravity Property

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Description

The vector representing the dry vehicle center of mass (i.e. no attached Tanks are included in this property) referenced from the origin of the Spacecraft's body fixed frame.. This property is used in calculating the CenterOfMass, which includes all attached Tanks in its calculation.

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/write
Units:	m
Default Value:	{ 0, 0, 0 }

Syntax

myVariable1 = mySpacecraft1.VehicleDryCenterOfGravity[0];

mySpacecraft1.VehicleDryCenterOfGravity[0] = myVariable1;