The article presents different methods of control of the lateral motion of aircraft during approach with the use of ILS‐LOC. Results of computer simulations are presented. An assessment of the quality with and without cross‐wind was made with the use of quality coefficients. The control laws are based on PID regulator and its modifications. Moreover, the application of the model‐following control in case of incomplete measurement, i.e. lack of information about the track angle, is presented. For interception, the model is used as the generator of the desired trajectory. The difference between the real and model trajectory is used for wind compensation, instead of the integration in LOC regulator. For control law synthesis for stabilization, linear quadratic regulator method was used. First Published Online: 14 Oct 2010


    Access

    Download


    Export, share and cite



    Title :

    Analysis of control quality of aircraft lateral motion during approach with the use of different control laws


    Contributors:


    Publication date :

    2006




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Analytical synthesis of control laws for lateral motion of aircraft

    Zubov, N. E. / Mikrin, E. A. / Ryabchenko, V. N. et al. | Online Contents | 2015


    Analytical synthesis of control laws for lateral motion of aircraft

    Zubov, N. E. / Mikrin, E. A. / Ryabchenko, V. N. et al. | Springer Verlag | 2015


    Control of the aircraft-on-ground lateral motion during low speed roll and manoeuvers

    Duprez, J. / Mora-Camino, F. / Villaume, F. | IEEE | 2004


    Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

    Zubov, N. E. / Mikrin, E. A. / Ryabchenko, V. N. et al. | Online Contents | 2017


    Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

    Zubov, N. E. / Mikrin, E. A. / Ryabchenko, V. N. et al. | Springer Verlag | 2017