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    LQR controller design for quad-rotor helicopters.

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    Authors
    E. Okyere
    A. bousbaine
    G. T. Poyi
    A.K. Joseph
    J.M. Andrade
    Affiliation
    University of Derby
    Issue Date
    2018-06-22
    
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    Abstract
    This paper presents an analysis and performance of a LQR control algorithm for quadrotor helicopters. For a successful analysis, first the dynamic model has been developed for the quadcopter and then the controller was designed, tuned and tested. In tuning the LQR, much attention was given to the feedback gain matrix (K). The controller’s performance wasverified in terms of delay time, rise time, overshoot, settling time and tolerance limits. The overall performance of theLQR controller was analysed.
    Citation
    Okyere, E., Bousbaine, A., Poyi, G. T., Joseph, A. K., and Andrade., J. M. (2018) ‘LQR controller design for quad-rotor helicopters’, The 9th International Conference on Power Electronics, Machines and Drives. The Arena and Convention Centre, Liverpool, 17-19 April. London: The Institute of Engineering and Technology, pp. 1-7.
    Publisher
    The Institute of Engineering and Technology.
    Journal
    The Journal of Engineering.
    URI
    http://hdl.handle.net/10545/623351
    Additional Links
    https://doi.org/10.1049/joe.2018.8126
    Type
    Article
    Meetings and Proceedings
    Language
    en
    Collections
    Department of Electronics, Computing & Maths

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