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Path: Orbit/OrbitCoord
% Scales CRTBP Jacobi coordinates to km and sec
Scales coordinates from Jacobi coordinates of the Circular Restricted Three
Body Problem to units of kilometers and seconds
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Form:
[stateOut,sec2tu] = CRTBP2kms(stateIn,distanceUnit,muPrimary,muSecondary);
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InputsP
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stateIn (1,6) Initial state vector
distanceUnit (1) Distance between Primary and Secondary bodies
(km)
muPrimary (1) Gravitational Parameter of Primary body
muSecondary (1) Gravitational Parameter of Secondary body
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Outputs
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stateOut (1,6) Output state vector
sec2tu (1) Scaling factor for time
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