Abstract Orbit selection is a necessary factor in nanosatellite formation mission design/meanwhile, to keep the formation, it is necessary to consume fuel. Therefore, the best orbit design for nanosatellite formation flying should be one that requires the minimum fuel consumption. The purpose of this paper is to analyse orbit selection with respect to the minimum fuel consumption, to provide a convenient way to estimate the fuel consumption for keeping nanosatellite formation flying and to present a simplified method of formation control. The formation structure is disturbed by J 2 gravitational perturbation and other perturbing accelerations such as atmospheric drag. First, Gauss’ Variation Equations (GVE) are used to estimate the essential Δ V due to the J 2 perturbation and atmospheric drag. The essential Δ V presents information on which orbit is good with respect to the minimum fuel consumption. Then, the linear equations which account for J 2 gravitational perturbation of Schweighart–Sedwick are presented and used to estimate the fuel consumption to maintain the formation structure. Finally, the relative dynamics motion is presented as well as a simplified motion control of formation structure by using GVE.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Relative dynamics and motion control of nanosatellite formation flying


    Beteiligte:
    Pimnoo, Ammarin (Autor:in) / Hiraki, Koju (Autor:in)

    Erschienen in:

    Advances in Space Research ; 57 , 7 ; 1476-1493


    Erscheinungsdatum :

    2016-01-06


    Format / Umfang :

    18 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Formation Flying and Relative Navigation - A Nanosatellite Research Mission (AAS 00-061)

    Chavez, F. R. / Schmidt, D. K. / American Astronautical Society | British Library Conference Proceedings | 2000



    Relative motion coupled control for formation flying spacecraft via convex optimization

    Wu, Yun-Hua / Cao, Xi-Bin / Xing, Yan-Jun et al. | Elsevier | 2010