To study the terminal guidance problem of maneuvering vehicle under the multiple constraints, an optimal guidance law is proposed. Considering of the terminal position, impact angle constraint and overload requirement. Firstly, the linear dynamic model of terminal guidance is established, and the expression of acceleration command is inferred by the Schwartz inequality theorem, then the form which is convenient for engineering application is presented. The features of guidance coefficient is obtained by analyzing the influence of guidance order to overload and trajectory characteristics. At last, the terminal guidance law is proposed. It is showed that the guidance law can both reduce the overload, and meet the command of maneuvering, impact angle constraint and attack accuracy by simulations.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Research of Terminal Optimal Guidance Law of MANEUVERING vehicle with Multiple Constrains


    Contributors:
    Qiang, Li (author) / Jun, Li (author) / Yonghai, Wang (author) / Xi, Zhang (author) / Xuguo, Qin (author)


    Publication date :

    2019-07-01


    Size :

    441897 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Optimal Guidance with Maneuvering Targets

    ROBERT B. ASHER AND JOHN P. MATUSZEWSKi | AIAA | 1974


    On the Optimal Estimator of Randomly Maneuvering Targets for Terminal Guidance

    Shinar, J. / International Federation of Automatic Control | British Library Conference Proceedings | 2004


    Real-time optimal guidance for orbital maneuvering

    COHEN, A. / BROWN, K. | AIAA | 1973


    Real-Time Optimal Guidance for Orbital Maneuvering

    AUDREY 0. COHEN AND KENNETH R. BROWN | AIAA | 1973


    Orbital maneuvering vehicle guidance, navigation and control

    Huber, W. G. / Finnell, W., III | NTRS | 1985