AbstractA new global approach for rendezvous Linear Quadratic controller design is presented in this paper. Instead of solving the algebraic Riccati equation, a continuous simulated annealing (SA) algorithm is used to design rendezvous LQ controller. Optimization of one automatic rendezvous controller with 18 design parameters is illustrated. The results show that the SA algorithm can locate the global solution effectively and robust, besides a great number of global solutions have been obtained by the SA. The SA has demonstrated better performance than other optimization algorithms such as floating-coded Genetic Algorithm, Simplex method and Powell algorithm.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Spacecraft optimal rendezvous controller design using simulated annealing


    Beteiligte:
    Luo, Ya-zhong (Autor:in) / Tang, Guo-jin (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2005-07-28


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Optimal Spacecraft Rendezvous Using Genetic Algorithms

    Young Ha Kim / David B. Spencer | AIAA | 2002



    Spacecraft Rendezvous

    Hintz, Gerald R. | Springer Verlag | 2023


    Spacecraft Rendezvous

    Hintz, Gerald R. | Springer Verlag | 2015