The invention discloses a flying wing unmanned aerial vehicle control surface fault tolerance method based on improved dynamic MOPSO, and belongs to the technical field of calculation, reckoning or counting. Aiming at the comprehensive characteristics of control surface redundancy, control surface limitation, strong coupling, strong nonlinearity and the like of the flying-wing unmanned aerial vehicle with advanced layout, the invention provides the fault tolerance method based on improved dynamic multi-target particle swarm control redistribution, so that the control surface characteristics of the flying-wing unmanned aerial vehicle are effectively processed, the influence of control surface faults during flight control is reduced, and the reliability of the flying-wing unmanned aerial vehicle is improved. And the stability and tracking precision of the control system are ensured.

    本发明公开了一种基于改进型动态MOPSO的飞翼无人机操纵面故障容错方法,属于计算、推算或计数的技术领域。本发明针对先进布局飞翼无人机的操纵面冗余、舵面受限、强耦合及强非线性等综合特性,提出基于改进型动态多目标粒子群控制重分配的故障容错方法,有效处理飞翼无人机的舵面特性,降低飞行控制时操纵面故障的影响,保证控制系统的稳定性和跟踪精度。


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    Titel :

    Flying wing unmanned aerial vehicle control surface fault tolerance method based on improved dynamic MOPSO


    Weitere Titelangaben:

    一种基于改进型动态MOPSO的飞翼无人机操纵面故障容错方法


    Beteiligte:
    ZHENG FENGYING (Autor:in) / XU MENGYUAN (Autor:in) / LI YAQIN (Autor:in)

    Erscheinungsdatum :

    2023-01-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen



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