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International Journal of Aerospace Engineering
Volume 2018, Article ID 2105682, 14 pages
https://doi.org/10.1155/2018/2105682
Research Article

Analysis of Global Sensitivity of Landing Variables on Landing Loads and Extreme Values of the Loads in Carrier-Based Aircrafts

College of Aerospace Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing, China

Correspondence should be addressed to Mingbo Tong; nc.ude.aaun@wgnot

Received 12 June 2017; Revised 26 October 2017; Accepted 9 November 2017; Published 14 January 2018

Academic Editor: Kenneth M. Sobel

Copyright © 2018 Jin Zhou et al. 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.

Linked References

  1. S. A. Shappell and D. F. Neri, The Effect of Combat on Aircrew Subjective Readiness and LSO Grades during Operation Desert Shield/Storm, Naval Aerospace Medical Research Lab, Pensacola, FL, USA, 1992.
  2. B. N. Acharya, G. P. Gupta, S. Prakash, and M. P. Kaushik, “UV-resistant, water repellent and rodent repellent nylon tapes for aircraft arrester system,” Pigment & Resin Technology, vol. 34, no. 5, pp. 270–274, 2005. View at Publisher · View at Google Scholar · View at Scopus
  3. D. T. Rusk, J. Pierce, W. Hoppe, B. Lancaster, R. Actis, and B. Szabo, Analysis and Testing of Fleet Corroded F/A-18C/D Arrestment Shanks, Naval Air Warfare Center Aircraft, Patuxent River, MD, USA, 2008.
  4. B. D. Flansburg, “Structural loads analysis of a carrier onboard delivery aircraft,” in 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, CA, USA, 2016. View at Publisher · View at Google Scholar
  5. N. S. Currey, Aircraft Landing Gear Design: Principles and Practices, American Institute of Aeronautics and Astronautics, Washington DC, USA, 1988.
  6. Landing gear design loads, Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine, France, 1991, AD-A239 914.
  7. Naval Air Systems Command, MIL-A-8863C (AS) Air-Plane Strength and Rigidity, Ground Loads for Navy Acquired Airplanes, Patuxent River, MD, USA, Naval Air Systems Command, 1993.
  8. Naval Air Systems Command, JSSG-2006 Aircraft Structures, Patuxent River, MD, USA, Naval air systems command, 1998.
  9. R. P. Micklos, Carrier Landing Parameters from Survey 45, Fleet and Training Command Aircraft Landing Aboard USS ENTERPRISE CVN-65 (Appendices B Through R), Naval Air Development Center, Warminster PA Air Vehicle and Crew Systems Technology Department, Warminster, PA, USA, 1991.
  10. Z. Wen, Z. Zhi, Z. Qidan, and X. Shiyue, “Dynamics model of carrier-based aircraft landing gears landed on dynamic deck,” Chinese Journal of Aeronautics, vol. 22, no. 4, pp. 371–379, 2009. View at Publisher · View at Google Scholar · View at Scopus
  11. D. Mikhaluk, I. Voinov, and A. Borovkov, Finite Element Modeling of the Arresting Gear and Simulation of the Aircraft Deck Landing Dynamics, 2011.
  12. L. Lihua, W. Chen, and X. Panpan, “Dynamic analysis of aircraft arresting gear based on finite element method,” in 2011 International Conference on System science, Engineering design and Manufacturing informatization, pp. 118–121, Guiyang, China, 2011. View at Publisher · View at Google Scholar · View at Scopus
  13. S. C. Sati, A. S. Kanaskar, S. R. Kajale, and A. Mukherjee, “Modeling, simulation and analysis of aircraft arresting system using bond graph approach,” Simulation Modelling Practice and Theory, vol. 19, no. 3, pp. 936–958, 2011. View at Publisher · View at Google Scholar · View at Scopus
  14. G. Sebastian, “Simulation of a free flight aircraft engagement during a carrier landing,” in 35th Structures, Structural Dynamics, and Materials Conference, Hilton Head, SC, USA, 1994, AIAA-1994-1619- CP. View at Publisher · View at Google Scholar
  15. D. H. Chester, “Aircraft landing impact parametric study with emphasis on nose gear landing conditions,” Journal of Aircraft, vol. 39, no. 3, pp. 394–403, 2002. View at Publisher · View at Google Scholar
  16. F. Yunwen, L. Sihong, X. Xiaofeng, C. Shuai, and P. Wenting, “Sinking velocity impact analysis of carrier-based aircraft based on test data,” Acta Aeronautica et Astronautica Sinica, vol. 36, no. 11, pp. 3578–3585, 2015. View at Google Scholar
  17. M. Zhang, H. Nie, and Z. H. He, “Optimization parameters of nose landing gear considering both take-off and landing performance of catapult take-off carrier-based aircraft,” Transactions of Nanjing University of Aeronautics & Astronautics, vol. 01, p. 12, 2016. View at Google Scholar
  18. A. Saltelli, S. Tarantola, and K. P.-S. Chan, “A quantitative model-independent method for global sensitivity analysis of model output,” Technometrics, vol. 41, no. 1, pp. 39–56, 1999. View at Publisher · View at Google Scholar
  19. M. Crosetto and S. Tarantola, “Uncertainty and sensitivity analysis: tools for GIS-based model implementation,” International Journal of Geographical Information Science, vol. 15, no. 5, pp. 415–437, 2001. View at Publisher · View at Google Scholar · View at Scopus
  20. C. Xu and G. Z. Gertner, “A general first-order global sensitivity analysis method,” Reliability Engineering & System Safety, vol. 93, no. 7, pp. 1060–1071, 2008. View at Publisher · View at Google Scholar · View at Scopus
  21. N. H. Sandlin, R. S. Ebers, and R. Black, “Ship motion effects on landing impact loads<149>V/STOL landing on aircraft carrier,” in 20th Structures, Structural Dynamics, and Materials Conference, St. Louis, MO, USA, 1979, AIAA 79-0742. View at Publisher · View at Google Scholar
  22. I. F. Mondragon, P. Campoy, C. Martinez, and M. A. Olivares-Mendez, “3D pose estimation based on planar object tracking for UAVs control,” in 2010 IEEE International Conference on Robotics and Automation, pp. 35–41, Anchorage, AK, USA, 2010. View at Publisher · View at Google Scholar · View at Scopus
  23. L. Kege and Y. Chuliang, “Load measurement and compilation of landing gear of airplane,” Acta Aeronautica et Astro-nautica Sinica, vol. 32, pp. 841–848, 2011. View at Google Scholar