In the modern battlefield, traditional guidance law like PNG can’t meet the needs of specific tasks. In this paper, we take terminal angle and flight time into consideration. Firstly, we use optimal control to satisfy impact angle requirement. Then, flight time error is designed to control impact time. Consider large errors caused by using the traditional estimator of time-to-go to attack maneuvering target, an improved time-to-go estimator is designed. Numerical simulations show excellent results of the devised law.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Time and Angle Constraint Guidance Law Applicable to Maneuvering Target


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Chen, Ye (Autor:in) / Guo, Zhengyu (Autor:in) / Cai, Yunze (Autor:in)


    Erscheinungsdatum :

    30.10.2021


    Format / Umfang :

    12 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Time and Angle Constraint Guidance Law Applicable to Maneuvering Target

    Chen, Ye / Guo, Zhengyu / Cai, Yunze | TIBKAT | 2022


    Time and Angle Constraint Guidance Law Applicable to Maneuvering Target

    Chen, Ye / Guo, Zhengyu / Cai, Yunze | British Library Conference Proceedings | 2022


    Optimal sliding mode guidance law against maneuvering target with impact angle constraint

    Gong, Mian / Zhou, Siteng / Zhou, Di | SAGE Publications | 2024



    Fixed-Time Terminal Angle-Constrained Cooperative Guidance Law Against Maneuvering Target

    Dong, Wei / Wang, Chunyan / Wang, Jianan et al. | IEEE | 2022