A strategy for trajectory design, motion camouflage, is introduced within the context of orbital relative motion. At first the equations of orbital motion for this approach are developed. The control strategy is then implemented using both an impulsive and continuous approach. A number of parameters are then optimized to minimize the fuel mass. The simulation results reveal that the predator successfully reaches the target and thus proving the validity of this approach.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Motion camouflage for in-orbit maneuvers


    Contributors:
    Tao Yang, (author) / Radice, G (author) / Weihua Zhang, (author)


    Publication date :

    2010-06-01


    Size :

    745036 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Viking Orbit Trim Maneuvers

    G.R. Hintz / D.L. Farless / M.J. Adams | AIAA | 1980



    Orbit Maneuvers Through Inter-Satellite Forcing

    Norman, Michael / Peck, Mason | AIAA | 2009


    Orbit Maneuvers Through Inter-Satellite Forcing

    Norman, M. / Peck, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Analytical Sun-Synchronous Low-Thrust Orbit Maneuvers

    Docherty, Stephanie Y. / Macdonald, Malcolm | AIAA | 2012