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Extended incremental nonlinear dynamic inversion for optical flow control of micro air vehicles

机译:微空气汽车光流量控制的扩展增量非线性动态反转

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摘要

Optical flow-based control strategies have always inspired robotic scientists, especially those in the field of Micro Air Vehicles (MAVs), thanks to their computational efficiency and relative simplicity. A major problem is that the success of optical flow control is governed by the availability of distance estimates, while optical flow provides only the ratio of velocity to distance. Therefore, with only monocular visual information, the inherent nonlinearity of optical flow observables has imposed several challenges in the controller design. In this paper, we propose a newly formulated controller, Extended Incremental Nonlinear Dynamic Inversion (EINDI), to deal with nonlinearities in the system output, such as optical flow control problems. The proposed method unlocks the potential of its predecessor (INDI) in output feedback control by removing the common assumption of time-scale separation, allowing internal dynamics to exist, and requiring only the input and output measurements. Furthermore, the EINDI method has been implemented on an MAV and tested successfully for optical flow landing in a simulation and a real-world outdoor environment. Both simulation and flight test results show 1) good tracking performance of the EINDI control compared to the conventional feedback control, 2) smooth landing trajectories without any oscillation, and 3) fast adaptation of the EINDI control even for landings at different heights and desired setpoints. (C) 2021 Elsevier Masson SAS. All rights reserved.
机译:光学流量的控制策略始终启发机器人科学家,特别是由于其计算效率和相对简单性,尤其是微型航空器(MAVS)领域的机器人科学家。主要问题是光学流量控制的成功通过距离估计的可用性来控制,而光学流量仅提供速度与距离的比率。因此,只有单眼视觉信息,光学流动可观察到的固有非线性在控制器设计中施加了若干挑战。在本文中,我们提出了一种新配制的控制器,扩展增量非线性动态反转(EINDI),以处理系统输出中的非线性,例如光学流量控制问题。该方法通过去除时间尺度分离的公共假设来解锁其前身(INDI)的潜力,允许存在内部动态,并且仅需要输入和输出测量。此外,EINDI方法已经在MAV上实施,并在模拟和现实世界的户外环境中成功测试了光流降落。模拟和飞行试验结果表明,eindi控制的良好跟踪性能与传统的反馈控制相比,2)平滑的着陆轨迹没有任何振荡,3)即使对于不同高度和所需设定点的着陆,eindi控制的快速调整。 (c)2021 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2021年第9期|106889.1-106889.14|共14页
  • 作者单位

    Univ Sains Malaysia Sch Aerosp Engn Engn Campus Nibong Tebal 14300 Pulau Pinang Malaysia|Delft Univ Technol Fac Aerosp Engn Kluyverweg 1 NL-2629 HS Delft Zuid Holland Netherlands;

    Univ Sains Malaysia Sch Aerosp Engn Engn Campus Nibong Tebal 14300 Pulau Pinang Malaysia|Delft Univ Technol Fac Aerosp Engn Kluyverweg 1 NL-2629 HS Delft Zuid Holland Netherlands;

    Delft Univ Technol Fac Aerosp Engn Kluyverweg 1 NL-2629 HS Delft Zuid Holland Netherlands;

  • 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

    Optical flow; Extended incremental nonlinear dynamic inversion; Nonlinear adaptive control; Micro air vehicles; Output feedback;

    机译:光流;延长增量非线性动态反转;非线性自适应控制;微型空气车辆;输出反馈;

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