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Robust sliding mode guidance and control for soft landing on small bodies

机译:坚固的滑模引导和控制,可在小车身上进行软着陆

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摘要

The variable structure control (VSC) with sliding mode is presented to design a tracking control law to ensure the fast and accurate response and robustness of guidance law in this paper. First, the small body dynamic equation is deduced in the landing site coordinate system. Second, the desired trajectory is planned in the condition of safe soft landing constraints. Third, the guidance law based on VSC is designed to track the desired trajectory and succeed in landing on the surface of small body. Finally, the guidance and control algorithm is formed and the effectiveness of algorithm is verified by numerical Monte Carlo simulations.
机译:为了保证快速,准确的响应和鲁棒的制导律,提出了一种具有滑模的变结构控制(VSC)设计跟踪控制律。首先,在着陆点坐标系中推导出小物体动力学方程。其次,在安全的软着陆约束条件下计划期望的轨迹。第三,基于VSC的制导律旨在跟踪所需的轨迹并成功降落在小物体的表面上。最后,形成了制导控制算法,并通过数值蒙特卡洛仿真验证了算法的有效性。

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  • 来源
    《Journal of the Franklin Institute》 |2012年第2期|p.493-509|共17页
  • 作者单位

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

    Deep Space Exploration Research Center, School of Astronautics, Harbin Institute of Technology,Harbin 150001, China;

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  • 入库时间 2022-08-18 02:57:57

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