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SUPPORT SITE |
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SUPPORT SITE |
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Path: SpacecraftEstimation/DemoFuns
% Right-hand-side for a cartesian orbit.
t is not used. This is compatible with RK4 and RK45.
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Form:
f = RHSUKF( x, t, d )
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Inputs
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x (6,1) State [r;v]
t (1,1) Time (not used)
d (1,1) Data structure
.a (3,1) Acceleration
.mu (1,1) Gravitational parameter
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Outputs
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f (6,1) State derivative
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References: None
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Math: Linear/Mag
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