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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Adaptive Control with Explicit Parameter Identification for Tactical Missiles


    Contributors:

    Publication date :

    1971


    Size :

    122 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    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