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

Author:

Lin Zhonglin1ORCID,Wang Weixiong1,Li Yufeng1,Zhang Xinglong2ORCID,Zhang Tianhong2,Wang Haitao1,Wu Xianyu1ORCID,Huang Feng1

Affiliation:

1. School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou 350108, China

2. Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

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.

Funder

Funding of the Natural Science Foundation of Fujian Province of China

Funding of the 2020 Fujian Province Young and Middle-aged Teacher Education Research Project

Funding of the Fuzhou University Research Start-up Funding

Funding of the Crosswise Project of ‘Research on the Air Pressure Simulation System Design of Aero-engine Surge’

Publisher

MDPI AG

Subject

Aerospace Engineering

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Visual-based landing system of a multirotor UAV in GNSS denied environment;2023 IEEE 10th International Workshop on Metrology for AeroSpace (MetroAeroSpace);2023-06-19

2. Design and Implementation of UAV Semi-physical Simulation System Based on VxWorks;Lecture Notes in Electrical Engineering;2023

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