In all studies with content of harmonic perturbation effects on the spacecraft motion dynamics, main goal is to obtain a solution for optimization of the operation process, so that overshadowed mission costs. The case studies about this aim, mostly to the trajectory parameters optimization by considering the vehicle orbital conditions under various control methods is formed. While in this regards, the intrinsic properties of stable earth orbits and using them effectively is less than to analyze the problems is considered. The aspects of orbital geometry can remain virtually fixed over extended periods of time due to a natural phenomenon called a frozen orbit. Simulation algorithm has been achieved to solve this problem by extracting and combining the equations that govern the frozen conditions with the tangential forces (ΔV) equations for orbit correction. Simulation results show that, using frozen orbits condition results is preferable in considerable propellant saving, decrease Orbital Maintenance Maneuver (OMM), increase of accuracy position errors and thus performance improvement of the spacecraft for orbiter mission.


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    Titel :

    Evaluation of stable frozen orbit conditions in the spacecraft OMM reduction


    Beteiligte:
    Soleymani, A. (Autor:in) / Toloei, A. (Autor:in) / Shahsavari, H. (Autor:in)


    Erscheinungsdatum :

    2013-06-01


    Format / Umfang :

    1334216 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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