A framework is introduced to develop the theory of the adjoint method for models including both continuous and discrete dynamics. The basis of this framework consists of the class of impulsive linear dynamic systems. It allows extension of the adjoint method to more general models that include multirate subsystems or nonperiodic discrete events. Both the deterministic and the stochastic case are considered and the theory is applied to study the effect of uplinks on the performance of a guidance system. Presented as Paper 2009-6276 at the AIAA Guidance, Navigation, and Control Conference, Chicago, IL, 10-13 August 2009


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    Title :

    Adjoint Method for Hybrid Guidance Loop State-Space Models


    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



    Adjoint Method for Hybrid Guidance Loop State-Space Models

    Weiss, Martin / Bucco, Domenic | AIAA | 2015



    State-Space Approach to the Method of Adjoints for Hybrid Guidance Loop Models

    Weiss, M. / Bucco, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009