Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An Implementation Of An Inertially-Fixed Eigenaxis Attitude Maneuver Intercept Algorithm


    Beteiligte:

    Kongress:

    AIAA Guidance, Navigation and Control Conference and Exhibit



    Erscheinungsdatum :

    01.01.2008




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    An Implementation Of An Inertially-Fixed Eigenaxis Attitude Maneuver Intercept Algorithm

    Milenkovic, Z. / Martin, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    Near eigenaxis maneuver for on-orbit-servicing spacecraft

    Feng Wang, / Xibin Cao, / Xueqin Chen, et al. | IEEE | 2006


    Adaptive spacecraft attitude control utilizing eigenaxis rotations

    Cochran, J. E., Jr. / Colburn, B. K. / Speakman, N. O. | NTRS | 1975


    Near-Eigenaxis Rotation Control Law Design for Moving-to-Rest Maneuver

    Hwa-Suk Oh / Young-Deuk Yoon / Young-Keun Chang et al. | AIAA | 2001


    Space Station Zero Propellant Maneuver Flight Results Compared to Eigenaxis (AAS 08-108)

    Bedrossian, N. / Bhatt, S. / American Astronautical Society et al. | British Library Conference Proceedings | 2008