In this work, a coupling characteristic analysis for a waverider hypersonic flight test vehicle. For the face symetry hypersonic vehicle aerodynamic coupling problem is due to the angle of attack. The lateral/directional coupling stability, rolling control coupling stability and Weissman chart composite coupling effects were conducted on before the controller degsin. The coupling analysis indicated that the negative angle of attack flight condition had unstable risk. The navigation flight dynamic equation and 6DOF controller validate dynamic equation were illumminated, and the flight simulation model was developed. A standard simulation and zero-mean disturbance flight simulation were conducted. The results of the simulations are presented that the flight control laws were robust for disturbance.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Coupling characterization analysis and control system design of XK-2 waverider hypersonic vehicle


    Contributors:
    Feng Li, (author) / Chao Wang, (author) / Ning Zhang, (author) / Guidong Wang, (author)


    Publication date :

    2016-08-01


    Size :

    526190 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    A hypersonic waverider research vehicle

    HANEY, J. / CERVISI, R. / GRANTZ, A. et al. | AIAA | 1993



    Interactive design of hypersonic waverider geometries

    CENTER, K. / SOBIECZKY, H. / DOUGHERTY, F. | AIAA | 1991


    Aerodynamic analysis of hypersonic waverider aircraft

    Sandlin, Doral R. / Pessin, David N. | NTRS | 1993


    Waverider-based hypersonic projectiles

    EDQUIST, KARL / LEWIS, MARK | AIAA | 1993