A nonlinear three-dimensional all-aspect guidance problem of an acceleration-constrained missile is dealt with. The feedback linearization method is applied to derive a three-dimensional guidance law, which enables the missile to intercept a maneuvering target under all-aspect initial boresight and heading conditions. The new guidance law is characterized by convergence to a collision course. It is shown that the proposed guidance law enables interception where the proportional navigation and the augmented proportional navigation guidance laws fail. Simulations demonstrate that the proposed law has the capability to perform several interception trials.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    All-Aspect Three-Dimensional Guidance Law Based on Feedback Linearization


    Contributors:


    Publication date :

    2015




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.54 Flugführung
    Local classification TIB:    770/7040




    Nonlinear Three Dimensional Composite Guidance Law Based on Feedback Linearization

    Srivastava, Rituraj / Sarkar, A / Ghose, D et al. | AIAA | 2004


    AIAA-2004-4903 Nonlinear Three Dimensional Composite Guidance Law Based on Feedback Linearization

    Sarkar, A. / Ghose, D. / Gollakota, S. et al. | British Library Conference Proceedings | 2004


    Three-Dimensional Entry Guidance Using Exact Linearization

    Abe, A. / Shimada, Y. / Uchiyama, K. | British Library Conference Proceedings | 2006