Abstract This paper presents a guidance law that allows a vehicle to orbit around a target at a given radius using a side-bearing angle. The global asymptotic stability of the proposed method is demonstrated, and a linear analysis is performed to facilitate the proper selection of the relevant control parameter. Two flight experiments, one with a GPS-based flight control system and the other with a vision-based flight control system, are presented to demonstrate the feasibility and performance of the proposed guidance law.


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    Titel :

    Circumnavigation with Side-Bearing Angle


    Beteiligte:
    Park, Sanghyuk (Autor:in)


    Erscheinungsdatum :

    15.12.2017


    Format / Umfang :

    19 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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