This paper presents the results of attitude, velocity, heave and yaw controller design for an autonomous model scaled helicopter using identified model of vehicle dynamic from parameterized state-space model with quasi-steady attitude dynamic approximation (6 Degree of Freedom model). Multivariable state-space control methodology such as pole placement was used to design the linear state-space feedback for the stabilization of helicopter because of its simple controller architecture. The design specification for controller design was selected according to Military Handling Qualities Specification ADS-33C. Results indicate that acceptable controller can be designed using pole placement method with quasi-steady attitude approximation and it has been shown that the controller design was compliance with design criteria of hover requirement in ADS-33C.


    Access

    Download


    Export, share and cite



    Title :

    The Effectiveness of Pole Placement Method in Control System Design for an Autonomous Helicopter Model in Hovering Flight


    Contributors:

    Publication date :

    2009-12-30


    Remarks:

    International Journal of Integrated Engineering; Vol 1 No 3 (2009) ; 2600-7916 ; 2229-838X


    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Classification :

    DDC:    629 / 670



    Helicopter stability in hovering flight

    Payne, P.R. | Engineering Index Backfile | 1955


    Helicopter control and stability in hovering flight

    Miller, R.H. | Engineering Index Backfile | 1948



    H8 robust controller for autonomous helicopter hovering control

    Tijani, Ismaila B. | Online Contents | 2011


    Optimal Controller for an Autonomous Helicopter in Hovering and Forward Flight

    Zhao, L. / Murthy, V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009