This paper is to present a robust controller design method for developing autonomous landing systems of Unmanned Combat Air Vehicle (UCAV). We first analyze the characteristic of autonomous landing of UCAV, and put forward its landing performance specifications. Structure singular value μ| synthesis is used to develop autonomous landing systems to accurately follow the pre-designed ideal landing track or online generated optimal landing track. The robust performance of system is analyzed. The simulation results demonstrate that the designed autonomous landing system satisfies the performance requirements of autonomous landing of UCAV when there are uncertainties of UCAV aircraft model, measurement noises and exogenous disturbances.


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    Title :

    Research of autonomous landing control of unmanned combat air vehicle


    Contributors:
    Li, Shaoyan (author) / Chen, Zongji (author)

    Conference:

    Fifth International Symposium on Instrumentation and Control Technology ; 2003 ; Beijing,China


    Published in:

    Publication date :

    2003-09-02





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Research of autonomous landing control of unmanned combat air vehicle [5253-162]

    Li, S. / Chen, Z. / SPIE - The International Society for Optical Engineering | British Library Conference Proceedings | 2003



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