In order to improve the stability and the rapidity of Fixed-Altitude unmanned helicopter flight control system, this paper improves the control performance of the closed-loop system by establishing the dynamic mathematical model of unmanned helicopter and adjusts the parameters of the controller under guidance, and completes the simulation with MATLAB. Through the performance evaluation and series, feedback correction, and improved system performance, a quality improvement of unmanned helicopter Fixed-Altitude flight is obtained. This method can reduce the modeling workload and difficulty effectively, and express the process of unmanned helicopter Fixed-Altitude flight intuitively.


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    Title :

    Design and Simulation of a Kind of Unmanned Helicopter Fixed-Altitude Flight Control System


    Contributors:
    Ma, Wenlai (author) / Zhu, Shouxi (author) / Xue, Hongfang (author)


    Publication date :

    2014


    Size :

    10 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







    Automatic Flight Control System for an Unmanned Helicopter System Design and Flight Test Results

    Weidel, M. / Alles, W. / Advisory Group for Aerospace Research and Development; Flight Mechanics Panel | British Library Conference Proceedings | 1995