Abstract This paper investigates the velocity-free spacecraft pose tracking control in terms of dual quaternions, and its application to six-degrees-of-freedom (six-DOF) asteroid-hovering operation. First, a coupled linear velocity and angular velocity observer, driven by the spacecraft position and attitude measurements, is designed via the immersion and invariance (I&I) methodology. After dominating the nonlinear terms in the pose dynamics due to rotation motion by high-gain injection, the observer is shown to be exponentially convergent. An output-feedback pose tracking law is then derived by combining the proposed velocity observer and a full-state feedback proportional-derivative controller with a proven separation principle. Finally, an asteroid hovering operation with the proposed method is simulated to demonstrate its effectiveness and application.

    Highlights The spacecraft pose control without velocity measurements is addressed. A global exponential velocity observer is designed to estimate spacecraft velocity. A novel velocity-free pose tracker is derived using the proposed velocity observer.


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    Titel :

    Dual-quaternion immersion and invariance velocity observer for controlling asteroid-hovering spacecraft


    Beteiligte:
    Dang, Qingqing (Autor:in) / Gui, Haichao (Autor:in) / Xu, Ming (Autor:in) / Wen, Hao (Autor:in)

    Erschienen in:

    Acta Astronautica ; 161 ; 304-312


    Erscheinungsdatum :

    2019-04-22


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch








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