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author:

Lin, Zhonglin (Lin, Zhonglin.) [1] (Scholars:林忠麟) | Wang, Weixiong (Wang, Weixiong.) [2] | Li, Yufeng (Li, Yufeng.) [3] | Zhang, Xinglong (Zhang, Xinglong.) [4] | Zhang, Tianhong (Zhang, Tianhong.) [5] | Wang, Haitao (Wang, Haitao.) [6] | Wu, Xianyu (Wu, Xianyu.) [7] (Scholars:吴衔誉) | Huang, Feng (Huang, Feng.) [8]

Indexed by:

Scopus SCIE

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 x 2 x 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 degrees, the repeated positioning accuracy of the three-axis translation table reaches 0.033 mm, and the dynamic-positioning accuracy reaches 0.04 degrees and 0.4 mm, which meets the simulation requirements of high-precision visual UAV navigation.

Keyword:

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

Community:

  • [ 1 ] [Lin, Zhonglin]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R China
  • [ 2 ] [Wang, Weixiong]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R China
  • [ 3 ] [Li, Yufeng]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R China
  • [ 4 ] [Wang, Haitao]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R China
  • [ 5 ] [Wu, Xianyu]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R China
  • [ 6 ] [Huang, Feng]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R China
  • [ 7 ] [Zhang, Xinglong]Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
  • [ 8 ] [Zhang, Tianhong]Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China

Reprint 's Address:

  • [Huang, Feng]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350108, Peoples R 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 Discipline: ENGINEERING;

ESI HC Threshold:35

JCR Journal Grade:2

CAS Journal Grade:2

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count: 2

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 2

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