A generic guidance design framework is proposed that is based on the idea of minimizing the guidance effort expressed as the quadratic integral of the guidance command and imposing performance constraints on various trajectory parameters at arbitrary points in time during the flight. This framework extends previous work on guidance algorithms for active aerial defense and for obstacle avoidance. Using some concrete examples it is shown that the proposed framework is flexible enough to tackle interesting guidance problems related to multiple targets scenarios. It is also shown that the same framework offers a practical solution for the optimal intercept guidance problem with constraints on the lateral missile acceleration.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Linear Quadratic Minimum-Effort, Specify-Performance Approach to Missile Guidance


    Beteiligte:
    Weiss, Martin (Autor:in) / Shima, Tal (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2020-11-25


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Minimum-Effort Guidance Using Quadratic Kinematics Approximation

    Merkulov, Gleb / Weiss, Martin / Shima, Tal Y. | TIBKAT | 2022


    Minimum-Effort Guidance Using Quadratic Kinematics Approximation

    Merkulov, Gleb / Weiss, Martin / Shima, Tal Y. | AIAA | 2022


    A Generic Guidance Design Method Based on Minimum Quadratic Guidance Effort

    Weiss, Martin / Shima, Tal | British Library Conference Proceedings | 2019


    Minimum-Effort Impact-Time Control Guidance Using Quadratic Kinematics Approximation

    Merkulov, Gleb / Weiss, Martin / Shima, Tal | AIAA | 2021


    Minimum-Effort Waypoint-Following Guidance

    He, Shaoming / Lee, Chang-Hun / Shin, Hyo-Sang et al. | AIAA | 2019