Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Model Verification of a Satellite with Large Flexible Appendages for Control System Design (AIAA 2018-0209)


    Contributors:

    Conference:

    Space Flight Mechanics (Meeting)



    Publication date :

    2018-01-01


    Size :

    25 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Control Recovery of a Satellite with Flexible Appendages after Space Debris Impact (AIAA 2018-2099)

    Gransden, Derek I. / Mooij, Erwin | British Library Conference Proceedings | 2018


    Simulation of Icing on a Cascade of Stator Blades (AIAA-2006-0209)

    Lee, S. / Loth, E. / Broeren, A. et al. | British Library Conference Proceedings | 2006


    AIAA-2004-5348 Neural Optimal Attitude Controller for a Satellite with Flexible Appendages

    Gili, P. / Massotti, L. / Battipede, M. | British Library Conference Proceedings | 2004


    Helios Simulation of Rotors in Hover: The Boeing Company (AIAA 2014-0209)

    Tadghighi, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014