A compensating method for unbalance torque resulted from the platform deforming of the air-bearing spacecraft simulator acted on gravity is presented, that is making a tiny distance between the mass-center and the center of rotation of the platform in the vertical direction so as to offset the unbalance torque resulted from the shift the mass-center with respect to the center of rotation of the platform and from the platform deforming when acted on gravity in the maximum work range of two horizontal Eulerian angle. The change trend of maximum unbalance torque after compensated is discussed by the theory on spacecraft altitude kinetics. It is demonstrated that this method can be applied to any case that the air-bearing spacecraft simulator rotate around the horizontal axis. The result shows the maximum unbalance torque after compensated is only 1/25 little than the one before compensated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A new method for the compensation of unbalance torque of 3-DOF spacecraft attitude control simulator


    Beteiligte:
    Yanbin Li, (Autor:in) / Gang Bao, (Autor:in) / Zuwen Wang, (Autor:in)


    Erscheinungsdatum :

    2006-01-01


    Format / Umfang :

    413053 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Torque-saturated, Inertia-Free Spacecraft Attitude Control

    Cruz, G. / Yang, X. / Weiss, A. et al. | British Library Conference Proceedings | 2011


    Torque-saturated, Inertia-Free Spacecraft Attitude Control

    Cruz, Gerardo / Yang, Xuebo / Weiss, Avishai et al. | AIAA | 2011


    Efficient Control Torque Distribution Approach for Spacecraft Attitude Control

    Choi, Yoonhyuk / Leeghim, Henzeh / Bang, Hyochoong | AIAA | 2008