RHSSNP:
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Spacecraft with 4 RWA's and 2 solar arrays.
Since version 1.
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Form:
xDot = RHSSNP( x, t, inr, invInr, tExt, inrW, uW, tW, eSAC )
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Inputs
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x (15,1) The state vector
t Time
inr (3,3) Inertia
invInr (3,3) Inverse inertia
tExt (3,1) External torque
inrW (6) [SA,RWA] inertias
uW (3,6) [SA,RWA] unit vectors
tW (6) [SA,RWA] torque
eSAC (2) Solar array commanded angle (always one step)
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Outputs
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xDot (15,1) The derivative of the state vector
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Children:
AeroUtils: Coord/QIToBDot
SC: Dynamics/GSModel
