Abstract The problem of stabilizing the spacecraft orbit attitude was solved analytically for the sixth order model of its rotary motion with the use of the output feedback control synthesis that is based on decomposition of a control object. Numerical simulation data are presented.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity


    Beteiligte:
    Zubov, N. E. (Autor:in) / Mikrin, E. A. (Autor:in) / Ryabchenko, V. N. (Autor:in) / Sorokin, I. V. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 61 , 2 ; 201-211


    Erscheinungsdatum :

    2018-04-01


    Format / Umfang :

    11 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Attitude stabilization of rigid spacecraft with angular velocity and torque limitations

    Cheng, Chun-hua / Li, Lin / Han, Qiang et al. | Elsevier | 2021


    Angular Velocity Vector Determination of Spacecraft in Flat-Spin Attitude States

    Blacketer, Laurence | British Library Conference Proceedings | 2022


    Attitude Maneuver of Spacecraft With Angular Velocity Constraint

    Shi, Yongxia / Hu, Qinglei / Guo, Lei | IEEE | 2018


    Adaptive Attitude Control of Uncertain Spacecraft with Attitude and Angular Velocity Constraints

    Kang, Zeyu / Wu, Shufan / Wang, Xiaoliang et al. | British Library Conference Proceedings | 2023