DeltaEl2Alfriend:
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Compute Alfriend differential elements from standard differential elements.
Since version 7.
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Usage:
[dElA,T] = DeltaEl2Alfriend( e, w, M, dEl );
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Inputs
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e (1) Eccentricity
w (1) Argument of perigee [rad]
M (1) Mean anomaly [rad]
dEl (1,6) Orbital element differences [a,i,W,w,e,M]
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Outputs
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dElA (1,6) Orbital element differences [a,th,i,q1,q2,W]
T (6,6) Transformation matrix
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Children:
Math: Trigonometry/UnwrapPhase
OrbitMiniToolbox: Support/M2Nu