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Barrier Lyapunov function-based robust flight control for the ultra-low altitude airdrop under airflow disturbances

机译:基于屏障Lyapunov功能的鲁棒飞行控制,用于气流扰动下的超低空空投

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摘要

This paper investigates the anti-disturbance constrained trajectory flight control for the ultra-low altitude airdrop under airflow disturbances, by innovatively integrating the finite time convergent high-order sliding mode observer and barrier Lyapunov function-based back-stepping technique. The dynamics of transport aircraft during the airdrop are established based on the fixed-wing aircraft's 6 DOF nonlinear model and are transformed into the affine nonlinear form for the convenient control design. These dynamics include the complex influence of the flow disturbances, the ground effect, the consecutive movement and abrupt extraction of the heavy cargo. Then, the flight controller is divided into several cascade subsystems via back-stepping technique. The items reflect the disturbances during the drop in each subsystem, as well as the items which are independent of the predefined virtual control variables, are taken as components of the "lumped disturbances" which are estimated and compensated by the specially designed finite time convergent high order sliding mode observer. On this basis, a barrier Lyapunov function-based back-stepping flight controller is proposed for the robust and safe flight control of the ultra-low altitude airdrop. And the closed-loop stability is discussed via the Lyapunov stability theorem. Simulation comparisons are conducted to verify the robustness and effectiveness of the proposed airdrop flight control method. (C) 2018 Elsevier Masson SAS. All rights reserved.
机译:通过创新性地整合了有限时间收敛的高阶滑模观测器和基于屏障李雅普诺夫函数的后推技术,研究了气流扰动下超低空空投的反干扰约束轨迹飞行控制。根据固定翼飞机的6自由度非线性模型建立运输飞机在空投过程中的动力学特性,并将其转换为仿射非线性形式,以便于控制设计。这些动力学因素包括流扰动,地面效应,重物的连续运动和突然提取的复杂影响。然后,通过反步技术将飞行控制器分为几个级联子系统。这些项目反映了每个子系统在下降期间的干扰,并且与预定义虚拟控制变量无关的项目被视为“集中干扰”的组成部分,这些“集中干扰”通过特殊设计的有限时间进行估算和补偿会聚高阶滑模观测器。在此基础上,为实现超低空空投的鲁棒性和安全性,提出了一种基于李雅普诺夫功能障碍的后退飞行控制器。并通过李雅普诺夫稳定性定理讨论了闭环稳定性。进行了仿真比较,以验证所提出的空投飞行控制方法的鲁棒性和有效性。 (C)2018 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2019年第1期|375-386|共12页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Jiangsu, Peoples R China|Nanjing Univ Aeronaut & Astronaut, Flight Control Res Inst, Nanjing 211106, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Jiangsu, Peoples R China|Nanjing Univ Aeronaut & Astronaut, Flight Control Res Inst, Nanjing 211106, Jiangsu, Peoples R China;

    Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Airdrop; Aircraft; Flight control; Barrier Lyapunov function; High order sliding mode;

    机译:空投;飞机;飞行控制;屏障李雅普诺夫功能;高阶滑模;

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