Open Access
Issue
MATEC Web Conf.
Volume 179, 2018
2018 2nd International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2018)
Article Number 03022
Number of page(s) 9
Section Aerospace
DOI https://doi.org/10.1051/matecconf/201817903022
Published online 26 July 2018
  1. Bacic M, Daniel R. Towards a low-cost hardware-in-the-loop simulator for free flight simulation of unmanned air vehicles. AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA 2005-6102, 2005. [Google Scholar]
  2. Bacic M, Daniel R. Hardware-in-the-loop simulation of aerodynamic objects. AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA 2007-6465, 2007. [Google Scholar]
  3. Papageorgiou G, Glover K. Two-degree-of-freedom control of an actively controlled wind-tunnel model. Journal of Guidance Control and Dynamics, 2002, 25(3): 510-516. [CrossRef] [Google Scholar]
  4. Richardson T S, Dubs A, Lowenberg M H, Jones C D. Wind-tunnel testing of a dynamic state-feedback gain scheduled control system. AIAA 2005-5976, 2005. [Google Scholar]
  5. Sohi N P. Modeling of spin modes of supersonic aircraft in horizontal wind tunnel. 24th International Congress of the Aeronautical Sciences, 2004. [Google Scholar]
  6. Gans N R, Dixon W E, Lind R, Kurdila A. A hardware in the loop simulation platform for vision-based control of unmanned air vehicles. Mechatronics, 2009, 19(2009): 1043-1056. [Google Scholar]
  7. Hu J, Li Q. Primary investigation of the virtual flight testing techniques in wind tunnel. Journal of Experiments in Fluid Mechanics, 2010, 24(1): 95-99. (in Chinese) [Google Scholar]
  8. Li H. Study on the similarity critiria and simulation method of the wind tunnel based virtual flight testing. PhD Thesis, China Aerodynamics Research and Development Center, 2012. (in Chinese) [Google Scholar]
  9. Zhao Z L, Wu J Q, L H, Zhou W Q, Mao D Y, Yang H Y. Investigation of virtual flight testing technique based on 2.4m transonic wind tunnel. Acta Aeronautica et Astronautica Sinica, 2016, 37(2): 504-512. (in Chinese) [Google Scholar]
  10. Nie B W, Zhu M H, Guo L L, Wen Y C, Jiang M. Key technique and design scheme of the wind tunnel virtual flight system. 2012 Chinese guidance, navigation and control conference (CGNCC2012), Beijing, 2012. (in Chinese) [Google Scholar]
  11. Lawrence C, Mills B. Status update of the AEDC virtual flight testing development program. AIAA 2002-0168, 2002. [Google Scholar]
  12. Magill J C, Cataldi P, Morency J R, Hammer D X, Burgess R, Jeter E. Demonstration of a wire suspension for wind-tunnel virtual flight testing. Journal of Spacecraft and Rockets, 2009, 46(3): 624-633. [CrossRef] [Google Scholar]
  13. Huang M, Wang Z W. A review of wind tunnel based virtual flight testing techniques for evaluation of flight control systems. International Journal of Aerospace Engineering, 2015(1), 1-22. [Google Scholar]
  14. Huang M, Wang Z W, Guo Z Y, Niu Y B. Design of the wind tunnel based virtual flight testing evaluation method for flight control systems. Proc IMechE Part G: Journal of Aerospace Engineering, 2016, 0(0): 1-13. [Google Scholar]
  15. Huang M, Wang Z W, Guo Z Y. Wind tunnel based virtual flight testing system and key technologies for the evaluation of flight control system. Journal of National University of Defense Technology, 2017, 39(2): 1-8. (in Chinese) [Google Scholar]
  16. Huang M, Wang Z W, Guo Z Y, Zeng Q H, Niu Y B. Wind tunnel hardware-in-the-loop simulation techniques for flight control system evaluation. 2017 2nd International Conference on Control, Automation and Artificial Intelligence, 2017. [Google Scholar]
  17. Zeng Q H, Guo Z Y. Unmanned flight control techniques and engineering. Beijing: National Defense Industry Press, 2011. (in Chinese) [Google Scholar]
  18. Gao J Y, Li L Y, Feng Y C, etc. Aircraft flight qualities. Beijing: National Defense Industry Press, 2011. (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.