The invention provides an adaptive control system for tailoring command or reference signals proportionally to available control actuator and sensor instrument acceleration rate and position capabilities. The invention can be used in a variety of applications, however, it has been developed and demonstrated in conjunction with guided missile airframe attitude control. In the guided missile applications wherein error signals are generated by comparing seeker attitude guidance or reference command signals with achieved attitude and control actuator deflection signals, the invention provides a means for generating adaptive control signals for tailoring the gain of the required command signals so that the capabilities of the control actuator, airframe and sensors are not exceeded.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Adaptive Control System Using Command Tailoring


    Contributors:

    Publication date :

    1973


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Tailoring Mission Operations and Command Assurance to TOPEX/POSEIDON

    Witkowski, M. / Hyman, S. / Bruno, K. et al. | NTRS | 1994


    Command Governor Based-adaptive Control

    Yucelen, T. / Johnson, E. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


    Command Governor-Based Adaptive Control

    Yucelen, Tansel / Johnson, Eric | AIAA | 2012