This paper presents a novel design of optimal flight control for a two-degree-of-freedom helicopter. The linear-quadratic-regulator (LQR) technology is applied to control the pitch motion of the helicopter. The particle swarm optimization (PSO) is employed to search the optimal weighting matrices of the LQR controller. Computer simulations demonstrate the flight performance will be optimal by means of the LQR control based on PSO.


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    Title :

    Optimal Design of Helicopter Control Systems Using Particle Swarm Optimization


    Contributors:


    Publication date :

    2019-05-01


    Size :

    273604 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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