RHSAlphaCentauriMission:
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Simple dynamical model for a flight to Alpha-Centauri.
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Form:
xDot = RHSAlphaCentauriMission( x, t, d )
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Inputs
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x (8,:) [r;v;m;center]
t (1,1) Time
d (1,1) Structure
.center (1,1) 1 = sun, 2 = alpha-centauri
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Outputs
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r (9,:) [rA;rB;rP]
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Children:
Math: Linear/Mag
Missions: AlphaCentauri/AlphaCentauriSystem
SC: Ephem/SunV1
