Path: Interplanetary/ThreeBody
% Compute linear system matrix for the circular restricted 3 body problem
Computes the matrix M such that
x = [r; v]
M = [ 0 I;
ddU K]
xDot = M*x
which is:
rDot = v
vDot = ddU*r + K*v
Type CRTBPLinarSystem for a demo.
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Form:
M = CRTBPLinearSystem( x, mu )
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Inputs
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x (6,1) Position and velocity in CRTBP system [r; v]
mu (1,1) Mass parameter
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Outputs
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M (6,6) Linear system state space matrix
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