Path: SC/Disturbances
% Computes a gravity gradient torque from r and mu.
q transforms from the frame in which r is defined to the body frame.
Since version 10.
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Form:
t = GravityGradientFromR( q, inr, r, mu )
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Inputs
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q (4,1) Quaternion from the r frame to Body
inr (3,3) Inertia matrix
r (3,:) Orbit from the earth to the spacecraft
in the spacecraft body frame (the same frame as
the inertia matrix.)
mu (1,1) Gravitational Parameter
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Outputs
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t (3,:) Torque (units will be consistent with inertia)
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AC: ACData/ACTConstants SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Quaternion/QForm Math: Linear/Cross Math: Linear/Mag
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