AbstractThe problem of the minimum time low-thrust transfer of a spacevehicle (SV) between arbitrary elliptic orbits in strong central Newtonian gravity field is under consideration. An approach is proposed to compute closer to optimal numerical solution of motion equations of a low-thrust SV, which realizes multiturn transfer. Both cases of variable and constant in magnitude rocket thrust are assumed. The examples of solutions of exact motion equations are given, which prove the validity of the proposed approach in combination with the use of the averaged solutions.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Quasioptimal interorbit transfers of a low-thrust spacecraft in strong central Newtonian gravity field


    Beteiligte:

    Erschienen in:

    Acta Astronautica ; 65 , 1-2 ; 82-94


    Erscheinungsdatum :

    2008-12-18


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Reducing Orbit Covariance for Continuous Thrust Spacecraft Transfers

    Zimmer, Scott / Ocampo, Cesar / Bishop, Robert | IEEE | 2010



    Minimum time transfers of a low-thrust rocket in strong gravity fields

    Kiforenko, Boris M. / Pasechnik, Zoya V. / Kyrychenko, Svitlana B. et al. | Elsevier | 2002