SPMDataF:
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Computes spin precession maneuver data for fuel budgets
Since version 1.
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Form:
x = SPMDataF( inr, cM, w, attI, attF, pwF, jD, thrusters )
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Inputs
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inr (1,1) Spin axis inertia
cM (3,1) Center of mass
w (3,1) Spin rate (rpm)
attI (1,2) Initial [ra,dec] (deg)
attF (1,2) Final [ra,dec] (deg)
pwF (1,1) Pulsewidth fraction
jD (1,1) Julian date
thrusters (1,n) Thruster IDs
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Outputs
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x (1,12+n) Formatted data
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Children:
SC: Attitude/RLP
SC: Ephem/SunV1
