The report discusses the design of an adaptive autopilot for a tactical missile. The subject autopilot explicitly identifies unknown, time-varying parameters and makes corresponding adjustments to autopilot feedback gains on the basis of a pole-assignment technique. The method of identification used is the extended Kalman filter. Effects of sensor measurement noise level, modeling uncertainties, autopilot input signal characteristics, and length of the measurement sampling interval are discussed. Identification accuracy is verified by computer simulation. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Adaptive Control with Explicit Parameter Identification for Tactical Missiles


    Beteiligte:
    C. F. Price (Autor:in) / W. D. Koenigsberg (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    122 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Lateral Jet Control for Tactical Missiles

    P. Champigny / R. G. Lacau | NTIS | 1994


    Lateral Jet Control for Tactical Missiles

    Champigny, P. / Lacau, R. G. / AGARD; Fluid Dynamics Panel | British Library Conference Proceedings | 1994


    Guidance and control of tactical missiles

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1972