We present a method to solve the impulsive minimum fuel maneuver problem for a distributed set of spacecraft. We develop the method assuming a non-linear dynamics model and parameterize the problem to allow the method to be applicable to multiple flight regimes including low-Earth orbits, highly-elliptic orbits (HEO), Lagrange point orbits, and interplanetary trajectories. Furthermore, the approach is not iimited by the inter-spacecraft separation distances and is applicable to both small formations as well as large constellations. We also apply a set of constraints to ensure that the fuel expenditure is equalized over the spacecraft in formation. We conclude with several examples and present optimal maneuver sequences for both a HE0 and libration point formation.


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    Titel :

    Direct Method for Fuel Optimal Maneuvers of Distributed Spacecraft in Multiple Flight Regimes


    Beteiligte:
    S. P. Highes (Autor:in) / D. S. Cooley (Autor:in) / J. J. Guzman (Autor:in)

    Erscheinungsdatum :

    2005


    Format / Umfang :

    34 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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