Abstract The lunar $ L_{1} $ and $ L_{2} $ libration points have been proposed as gateways granting inexpensive access to interplanetary space. To date, individual transfers between three-body systems have been determined. The methodology to solve the problem for arbitrary three-body systems and entire families of orbits is currently being studied. This paper presents an initial approach to solve the general problem for single and multiple impulse transfers. Two different methods of representing and storing the invariant manifold data are developed. Some particular solutions are presented for two types of transfer problems, though the emphasis is on developing the methodology for solving the general problem.


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    Title :

    Representations of Invariant Manifolds for Applications in Three-Body Systems


    Contributors:
    Howell, K. C. (author) / Beckman, M. (author) / Patterson, C. (author) / Folta, D. (author)


    Publication date :

    2006




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    Local classification TIB:    770/7040
    BKL:    55.60 Raumfahrttechnik




    Representations of Invariant Manifolds for Applications in Three-Body Systems

    Howell, K. C. / Beckman, M. / Patterson, C. et al. | Springer Verlag | 2006


    Representations of Invariant Manifolds for Applications in Three-Body Systems (AAS 04-287)

    Howell, K. / Beckman, M. / Patterson, C. et al. | British Library Conference Proceedings | 2005


    Use of Invariant Manifolds for Transfers Between Three-Body Systems

    Beckman, Mark / Howell, Kathleen | NTRS | 2003