Path: FormationFlying/Transformation
% Convert element differences to eccentric geometric goals.
Since version 7.
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Usage:
g = FFEccDeltaElem2Goals( el0, dEl, type );
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Inputs
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el0 (1,6) Initial reference orbital elements
dEl (1,6) Initial orbital element differences
type (1) Element set type
- 1 [a,theta,i,q1,q2,W] (Alfriend format)
- 2 [a,i,W,w,e,M] (standard format)
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Outputs
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g (.) Geometric goals data structure
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