Path: OpticalNavigation/Dynamics
% Right-hand-side for a 3 dimensional planet takeoff.
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Form:
d = RHSPlanet3D
xDot = RHSPlanet3D( x, ~, d )
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Inputs
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x (6,1) State vector [r;v]
t (1,1) Time (s) (unused)
d (.) Data structure
.acc (3,1) Thruster acceleration
.mu (1,1) Gravitational parameter
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Outputs
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xDot (6,1) d[r;v]/dt
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Math: Linear/Mag
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