Aerial vehicle landing is an open and challenging problem. This paper focuses on development of simple guidance laws for quadrotor landing with known GPS location - stationary and moving. The guidance laws are based on missile guidance principles, namely pure pursuit, line-of-sight, and pure proportional navigation. Comparison on the performance of these guidance laws is presented through Matlab simulations and ROS implementation.


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    Titel :

    Application of guidance laws to quadrotor landing


    Beteiligte:
    Gautam, Alvika (Autor:in) / Sujit, P.B. (Autor:in) / Saripalli, Srikanth (Autor:in)


    Erscheinungsdatum :

    01.06.2015


    Format / Umfang :

    2383751 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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