Open Access
Volume 37, Number 6, December 2019
Page(s) 1138 - 1147
Published online 11 February 2020
  1. O'Rourke M J. Simulation Model for Tail Rotor Failure[J]. Journal of Aircraft, 1994, 31(1): 197–205 [Article] [Google Scholar]
  2. Liu L, Pines D J. Analysis of US Civil Rotorcraft Accidents Caused by Vehicle Failure or Malfunction[C]//American Helicopter Society 61st Annual Forum Proceedings, Grapevine, 2005 [Google Scholar]
  3. Sun Jie, Gao Yanhui. The Helicopter Tail-Rotor Failure and the Flight Test[J]. Flight Mechanics, 2001, 19(4): 67–69 [Article] (in Chinese) [Google Scholar]
  4. Yu Qi, Zhang Haihong. Analysis of the Tail-Rotor Failure from Mechanical Malfunction and Research in Flight Test[J]. Flight Mechanics, 2008, 26(3): 74–77 [Article] (in Chinese) [Google Scholar]
  5. Frank L, Thongsay V. US Army Airworthiness Approval for UH-60 Fly-by-Wire Aircraft Flight Testing[C]//American Helicopter Society 66th Annual Forum, Arizona, 2010 [Google Scholar]
  6. Stacey K, David A. The Yaw Return Maneuver-the Regulatory History, Future, and Impact on the Structural Design Loads[C]//American Helicopter Society 65th Annual Forum, Grapevine, Texas, 2009 [Google Scholar]
  7. Singh H K, Pawar P M, Ganguli R, et al. On the Effect of Mass and Stiffness Unbalance on Helicopter Tail Rotor System Behavior[J]. Aircraft Engineering and Aerospace Technology, 2008, 80(2): 129–138 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  8. Li C G, Shu P, Ma X M, et al. Failure Analysis on Tailor Rotor Rod Components of a Helicopter[J]. Failure Analysis and Prevention, 2013, 8(6): 346–349 [Article] [Google Scholar]
  9. Goodman N, Bayoumi A, Blechertas V, et al. CBM Component Testing at the University of South Carolina: Ah-64 Tail Rotor Gearbox Studies[C]//AHS Technical Specialists' Meeting on Condition Based Maintenance Conference Proceedings, Virginia, 2009 [Google Scholar]
  10. Cherepinsky I, Driscoll J T, Kinkead W D, et al. Control Surface Failure Detection for Fly-by-Wire Aircraft[D]. U.S.Patent Application 8/032, 269[P]. 2011-10-4 [Google Scholar]
  11. Waltner P J, Knaust G. Tail Rotor Failure Recovery Controller[P]. U.S. Patent Application 10/124, 889, 2018-11-13 [Google Scholar]
  12. Somers T M, Bonino R K, Cleve B R, et al. HUMS/MMIS as an Aviation Combat Multiplier[C]//American Helicopter Society 63rd Annual Forum Proceedings, Virginia, 2007 [Google Scholar]
  13. Rajendran S, Gu D. Fault Tolerant Control of a Small Helicopter with Tail Rotor Failures in Hovering Mode[C]//11th IEEE International Conference on Control & Automation, 2014 [Article] [Google Scholar]
  14. Andrea R, Riccardo B M, Pietro S, et al. AW169 Loss of Tail Rotor Effectiveness Simulation[C]//43rd European Rotorcraft Forum, Forum, Milano, Italy, 2017 [Google Scholar]
  15. Bottasso C L, Maisano G, Scorcelletti F. Trajectory Optimization Procedures for Rotorcraft Vehicles, Their Software Implementation, and Applicability to Models of Increasing Complexity[J]. Journal of the American Helicopter Society, 2010, 55(3): 1–12 [Article] [CrossRef] [Google Scholar]
  16. Meng Wanli, Chen Renliang. Trajectory Optimization of Helicopter Autorotation Landing after One Engine Failure[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(9): 1599–1607 [Article] (in Chinese) [Google Scholar]
  17. Meng W, Chen R. Study of Helicopter Autorotation Landing Following Engine Failure Based on a Six-Degree-of-Freedom Rigid-Body Dynamic Model[J]. Chinese Journal of Aeronautics, 2013, 26(6): 1380–1388 [Article] [CrossRef] [Google Scholar]
  18. Meng Wanli. Study and Application of Trajectory Optimization for Helicopter Flight after One Engine Failure[D]. Nanjing, Nanjing University of Aeronautics and Astronautics, 2014: 13–33 (in Chinese) [Google Scholar]
  19. Gao Zheng, Chen Renliang. Helicopter Dynamics[M]. Beijing, Science Press, 2003: 168–184 (in Chinese) [Google Scholar]
  20. Yan Xufei, Chen Renliang. Helicopter Autorotation Landing Optimization after Tail-Rotor Total Failure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(6): 1203–1212 [Article] (in Chinese) [Google Scholar]
  21. Xin Hong, Gao Zheng. A Prediction of the Helicopter Vortex-Ring State Boundary[J]. Aerodynamic Experiment and Measurement & Control, 1996, 10(1): 14–19 [Article] (in Chinese) [Google Scholar]
  22. Betts J T. Survey of Numerical Methods for Trajectory Optimization[J]. Journal of Guidance Control & Dynamics, 1998, 21(2): 193–207 [Article] [Google Scholar]
  23. Kim S. Certification of Transport Category Rotorcraft[S]. 29-2C, Washington: Federal Aviation Administration, Department of Transportation, 2014: 57–146 [Google Scholar]
  24. Gill P E. User's Guide for SNOPT Version 7: Software for Large-Scale Nonlinear Programming[D]. San Diego, University of California, 2007 [Google Scholar]

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