Trajectory Design Combining Invariant Manifolds with Discrete Mechanics and Optimal Control
نویسندگان
چکیده
منابع مشابه
Trajectory Design Combining Invariant Manifolds with Discrete Mechanics and Optimal Control
ai = normalized radius of body’s circularized orbit for i M;S, where M moon and S sun C = cost function Cd = discrete cost function D1 D2 = operator that denotes the derivative with respect to the first (second) argument dEO = distance of spacecraft from Earth, km dMO = distance of spacecraft from moon, km dp = altitude of elliptical orbit at perigee, km E = energy integral Ei = critical energy...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2012
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.55426