An examination is made of the controlled motion of a dynamical system that is subject to interference and is described in the neighborhood of a nominal trajectory by a system of linear equations. It is assumed that the phase vector of the system can be measured exactly only at discrete instants of time. A procedure for constructing a control with simultaneous regard to deviations along two coordinates is proposed on the basis of two guaranteeing controls. This procedure is applied to the problem of constructing the control of an airplane in a vertical plane on landing, in the presence of wind disturbances. Such an approach enables deviations in altitude and vertical velocity simultaneously to be taken into account.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Quasioptimal correction of the motion of an airplane at landing when there are wind disturbances


    Weitere Titelangaben:

    Quasi-optimale Korrektur der Bewegung eines Flugzeuges bei der Landung bei Stoerungen durch Wind


    Beteiligte:
    Korneyev, V.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1987


    Format / Umfang :

    6 Seiten, 6 Quellen


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Quasioptimal Control of Space Redundant Manipulators

    Senda, K. / AIAA | British Library Conference Proceedings | 1999


    Airplane landing gear

    Maiorca, Salvatore | NTRS | 1931


    Airplane landing gear

    Engineering Index Backfile | 1943


    Airplane landing gear

    Maiorca, S. | Engineering Index Backfile | 1931