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International Journal of Aerospace Engineering
Volume 2015, Article ID 672423, 22 pages
http://dx.doi.org/10.1155/2015/672423
Review Article

A Review of Wind Tunnel Based Virtual Flight Testing Techniques for Evaluation of Flight Control Systems

Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, China

Received 8 June 2015; Revised 30 August 2015; Accepted 18 October 2015

Academic Editor: Paolo Tortora

Copyright © 2015 Min Huang and Zhong-wei Wang. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [11 citations]

The following is the list of published articles that have cited the current article.

  • Aziz Al-Mahadin, and Faouzi Bouslama, “Automatic identification of wake vortex traverse by transport aircraft using fuzzy logic,” 2017 IEEE 4th International Conference on Soft Computing & Machine Intelligence (ISCMI), pp. 133–139, . View at Publisher · View at Google Scholar
  • Min Huang, Zhong-wei Wang, Zhen-yun Guo, and Yao-bin Niu, “Design of the wind tunnel based virtual flight testing evaluation method for flight control systems,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 232, no. 1, pp. 17–29, 2016. View at Publisher · View at Google Scholar
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  • Ali Shakoori, Alexander Vladimirovich Betin, Denis Alexandrovich Betin, and Mahdi Mortazavi, “A novel method for moments of inertia tuning for free-flying dynamically similar models via simulated annealing,” International Journal of Technology, vol. 8, no. 3, pp. 376–386, 2017. View at Publisher · View at Google Scholar
  • Min Huang, Zhong-wei Wang, Xing-Bao Yang, Zhen-yun Guo, and Yao-bin Niu, “Preliminary Validation of the Wind Tunnel Based Flight Control System Evaluation Method,” MATEC Web of Conferences, vol. 179, pp. 03021, 2018. View at Publisher · View at Google Scholar
  • Xing-bao Yang, and Min Huang, “Evaluation Abilities and Requirements of the Wind Tunnel Hardware-in-the-loop Simulation for Evaluation of Missiles’ Flight Control Systems,” MATEC Web of Conferences, vol. 179, pp. 03022, 2018. View at Publisher · View at Google Scholar
  • Aziz Al-Mahadin, and Serdar Dalkilic, “Investigation of factors affecting aircraft vortex encounters,” 2018 Advances in Science and Engineering Technology International Conferences, ASET 2018, pp. 1–6, 2018. View at Publisher · View at Google Scholar
  • Lixin Wang, Xianshuai Zuo, Hailiang Liu, Xiaopeng Jia, Junbin You, and Ting Yue, “Flying qualities evaluation criteria design for scaled-model aircraft based on similarity theory,” Aerospace Science and Technology, 2019. View at Publisher · View at Google Scholar
  • Z. Gong, S. Araujo-Estrada, M. H. Lowenberg, S. A. Neild, and M. G. Goman, “Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig,” Journal of Aircraft, pp. 1–11, 2019. View at Publisher · View at Google Scholar