In this paper a systematic approach for weight selection has been applied. A classical phase lead compensator is used as weight (precompensator) in H infinity loop shaping for design of pitch controller for air vehicle. Analysis has been confined only to bode plots. The analysis and results achieved indicate that H infinity loop shaping control theory is a viable tool for design and synthesis of attitude control of air vehicle.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Weight selection in H- infinity loop shaping using lead/lag compensators


    Contributors:
    Ejaz, M. (author) / Arbab, M.N. (author) / Shah, S.W. (author)


    Publication date :

    2006


    Size :

    6 Seiten, 8 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Frequency-shaping with spatial compensators

    Smith, G. / Clark, Robert | AIAA | 2000


    Frequency-Shaping with Spatial Compensators

    Clark, R. / Smith, G. C. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000




    H-infinity loop shaping - The Bell 205 helicopter case study

    Smerlas, Alex / Postlethwaite, Ian / Walker, Daniel | AIAA | 1999