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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    Title :

    Application of guidance laws to quadrotor landing


    Contributors:


    Publication date :

    2015-06-01


    Size :

    2383751 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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