Large torque amplification and momentum storage capacity are the two basic properties that make control moment gyroscopes (CMGs) superior when compared to the reaction and momentum wheels commonly used in spacecraft attitude control. Software and Hardware in the Loop (HIL) tests are carried out for the verification of the requirements of CMG based attitude control systems (ACS). In order to have even a more realistic results, CMG based ACS HIL tests are performed on three axis air bearing test bed by taking into account the restrictions of the air bearing table used. The results of these simulations and tests are presented.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Verification of control moment gyroscopes based attitude control systems for agile satellite missions


    Contributors:
    Yavuzoglu, E. (author) / Topal, E. (author) / Kutlu, A. (author) / Urek, H. (author) / Gulluoglu, M. E. (author) / Tarakcioglu, O. (author) / Yurtoglu, E. (author) / Akin, D. (author) / Celik, K. (author) / Ozyurt, C. (author)


    Publication date :

    2011-06-01


    Size :

    1825620 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Steering Law of Control Moment Gyroscopes for Agile Attitude Maneuvers

    Kanzawa, Takuya / Haruki, Misuzu / Yamanaka, Koji | AIAA | 2016




    Controllability of spacecraft attitude using control moment gyroscopes

    Bhat, S.P. / Tiwari, P.K. | Tema Archive | 2009


    Torque Optimal Steering of Control Moment Gyroscopes for Agile Spacecraft

    Geshnizjani, Ramin / Kornienko, Andrei / Ziegler, Tobias et al. | AIAA | 2021