RHSCartesian:
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Right-hand-side for point-mass cartesian orbit with external acceleration.
Since version 7.
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Form:
xDot = RHSCartesian( t, x, d )
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Inputs
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t (1,1) Time
x (6,1) States [r;v]
d (1,1) Structure to pass to the integration RHS
.mu, gravitational parameter
.f, external acceleration, (3,1)
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Outputs
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xDot (3,1) State derivatives d[v]/dt
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Children:
Math: Linear/Mag
