Problems of nonlinear modeling, dynamic analysis and simulation of spatial motion by a spacecraft with a flexible weak damping structure, are considered. Attitude motion of a flexible spacecraft with pulse-width control, spin-up rotors of six single-gimbal control moment gyros (CMGs) at the initial, service and emergency modes, is studied. Results on analysis of the spacecraft nutation and flexible oscillations, are represented.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Spacecraft attitude pulse-width control at initial, service and emergency modes


    Contributors:

    Conference:

    9TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES: ICNPAA 2012 ; 2012 ; Vienna, Austria


    Published in:

    AIP Conference Proceedings ; 1493 , 1 ; 933-940


    Publication date :

    2012-11-06


    Size :

    8 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Spacecraft attitude pulse-width control at initial, service and emergency modes

    Somov, S. | British Library Conference Proceedings | 2012


    Passivity-Based Pulse-Width-Modulated Spacecraft Attitude Control

    Lang, Xiaoyu / de Ruiter, Anton | AIAA | 2021



    Spacecraft attitude guidance and economical digital control in initial modes

    Somova, Tatyana | American Institute of Physics | 2018


    Pulse motor for spacecraft attitude control.

    Blackwood, D. / Suddeth, D. | NTRS | 1968