The optimization of satellite orbits between the Earth and an asteroid when the satellite is powered by a low thrust ion drive or solar power unit was studied. It was assumed that the satellite is launched by an Ariane type launch vehicle. A hybrid Pontryagin/recursive quadratic programming approach was used. The software was developed on DEC System-10 computer and implemented on the ESOC Siemens 7865 Computer System. Results for 13 mission simulations are discussed.


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    Titel :

    Low Thrust Orbit Optimization for Interplanetary Missions, Volume 1


    Beteiligte:
    L. C. W. Dixon (Autor:in) / S. E. Hersom (Autor:in) / Z. A. Maany (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    117 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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