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[期刊论文]

Design and Experimental Study of a Novel Semi-Physical Unmanned-Aerial-Vehicle Simulation Platform for Optical-Flow-Based Navigation

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author:

Lin, Z. (Lin, Z..) [1] | Wang, W. (Wang, W..) [2] | Li, Y. (Li, Y..) [3] | Unfold

Indexed by:

Scopus

Abstract:

In the process of unmanned aerial vehicle (UAV) visual-navigation-algorithm design and accuracy verification, the question of how to develop a high-precision and high-reliability semi-physical simulation platform has become a significant engineering problem. In this study, a new UAV semi-physical-simulation-platform architecture is proposed, which includes a six-degree-of-freedom mechanical structure, a real-time control system and real-time animation-simulation software. The mechanical structure can realistically simulate the flight attitude of a UAV in a three-dimensional space of 4 × 2 × 1.4 m. Based on the designed mechanical structure and its dynamics, the control system and the UAV real-time flight-animation simulation were designed. Compared with the conventional simulation system, this system enables real-time flight-attitude simulation in a real physical environment and simultaneous flight-attitude simulation in virtual-animation space. The test results show that the repeated positioning accuracy of the three-axis rotary table reaches 0.006°, the repeated positioning accuracy of the three-axis translation table reaches 0.033 mm, and the dynamic-positioning accuracy reaches 0.04° and 0.4 mm, which meets the simulation requirements of high-precision visual UAV navigation. © 2023 by the authors.

Keyword:

optical flow semi-physical simulation platform six degrees of freedom unmanned aerial vehicle visual navigation

Community:

  • [ 1 ] [Lin, Z.]School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou, 350108, China
  • [ 2 ] [Wang, W.]School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou, 350108, China
  • [ 3 ] [Li, Y.]School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou, 350108, China
  • [ 4 ] [Zhang, X.]Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
  • [ 5 ] [Zhang, T.]Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
  • [ 6 ] [Wang, H.]School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou, 350108, China
  • [ 7 ] [Wu, X.]School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou, 350108, China
  • [ 8 ] [Huang, F.]School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou, 350108, China

Reprint 's Address:

  • [Huang, F.]School of Mechanical Engineering and Automation, China

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Source :

Aerospace

ISSN: 2226-4310

Year: 2023

Issue: 2

Volume: 10

2 . 1

JCR@2023

2 . 1 0 0

JCR@2023

ESI HC Threshold:35

JCR Journal Grade:2

CAS Journal Grade:2

Cited Count:

WoS CC Cited Count:

30 Days PV: 1

Affiliated Colleges:

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