Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    DUAL-QUATERNION BASED FINITE-TIME ADAPTIVE CONTROL FOR SPACECRAFT AUTONOMOUS PROXIMITY MANEUVER WITH PYRAMID-TYPE CONSTRAINTS


    Contributors:
    Wang, Liangyue (author) / Guo, Yanning (author) / Ma, Guangfu (author) / Lyu, Yueyong (author) / Zhang, Haibo (author)

    Conference:

    IAF Astrodynamics Symposium ; 2021 ; Dubai, Stadt



    Publication date :

    2022


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Robust Integrated Translation and Rotation Finite-Time Maneuver of a Rigid Spacecraft Based on Dual Quaternion

    Zhang, F. / Duan, G. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011


    Spacecraft Attitude Controller Design for Large Angle Maneuver Using Quaternion and Dual Mode Control

    Nam, H. S. / Kim, S. H. / Song, C. H. et al. | British Library Conference Proceedings | 1999


    Quaternion-based finite time control for spacecraft attitude tracking

    Wu, Shunan / Radice, Gianmarco / Gao, Yongsheng et al. | Elsevier | 2011