Skip to main navigation Skip to search Skip to main content

Robust component synthesis vibration suppression command for flexible spacecrafts with on-off actuators

    Research output: Chapters, Conference Papers, Creative and Literary WorksRGC 32 - Refereed conference paper (with host publication)peer-review

    Abstract

    This paper presents a development of component synthesis vibration suppression (CSVS) method for maneuvering flexible spacecrafts. The proposed method eliminates unwanted flexible vibrations while achieving the desired rigid body attitude motion. The robustness to uncertainties of dynamic modeling parameters is analyzed. Unlike traditional input shaping in which a numerical optimization is utilized, design for CSVS commands is based on analytic methodology and is relative easy to implement. A case study is performed on a time-fuel optimal control strategy using constant amplitude reaction thrusters. Both simulation and experimental results validate the effectiveness of the proposed approach.
    Original languageEnglish
    Title of host publicationProceedings - 2003 IEEE International Conference on Robotics, Intelligent Systems and Signal Processing, RISSP 2003
    PublisherIEEE
    Pages214-219
    Volume2003-October
    DOIs
    Publication statusPublished - 2003
    EventIEEE International Conference on Robotics, Intelligent Systems and Signal Processing, RISSP 2003 - Changsha, China
    Duration: 8 Oct 200313 Oct 2003

    Publication series

    Name
    Volume2003-October

    Conference

    ConferenceIEEE International Conference on Robotics, Intelligent Systems and Signal Processing, RISSP 2003
    PlaceChina
    CityChangsha
    Period8/10/0313/10/03

    Fingerprint

    Dive into the research topics of 'Robust component synthesis vibration suppression command for flexible spacecrafts with on-off actuators'. Together they form a unique fingerprint.

    Cite this