Spacecraft.GravityGradientTorque() Method

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Description

Calculates the gravity gradient torque acting on the spacecraft assuming a point mass model for the central body. The gravity gradient torque vector is referenced from the origin of the Spacecraft BCS.

 

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.

 

Method Signature

Spacecraft.GravityGradientTorque(

)

 

 

Return Value

Type:

Array of number (size = 3)

Units:

N m

 

 

Returns a vector corresponding to the torque about the spacecraft center of mass.

 

Syntax

myArray1 = mySpacecraft1.GravityGradientTorque();

 

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide