Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    An Implementation Of An Inertially-Fixed Eigenaxis Attitude Maneuver Intercept Algorithm



    Conference:

    Conference, Guidance, navigation and control ; 2008 ; Honolulu, HI



    Publication date :

    2008-01-01


    Size :

    12 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Near eigenaxis maneuver for on-orbit-servicing spacecraft

    Feng Wang, / Xibin Cao, / Xueqin Chen, et al. | IEEE | 2006


    Adaptive spacecraft attitude control utilizing eigenaxis rotations

    Cochran, J. E., Jr. / Colburn, B. K. / Speakman, N. O. | NTRS | 1975


    Near-Eigenaxis Rotation Control Law Design for Moving-to-Rest Maneuver

    Hwa-Suk Oh / Young-Deuk Yoon / Young-Keun Chang et al. | AIAA | 2001


    Space Station Zero Propellant Maneuver Flight Results Compared to Eigenaxis (AAS 08-108)

    Bedrossian, N. / Bhatt, S. / American Astronautical Society et al. | British Library Conference Proceedings | 2008