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SCIENCE CHINA Information Sciences, Volume 62, Issue 1: 010207(2019) https://doi.org/10.1007/s11432-018-9580-3

Taxiing stability verification and airworthiness certification for amphibious aircraft

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  • ReceivedJul 4, 2018
  • AcceptedJul 16, 2018
  • PublishedDec 14, 2018

Abstract

There is no abstract available for this article.


Acknowledgment

The authors thank the AVIC Landing Gear Advanced Manufacturing Corporation and SIEMENS PLM Software Inc. for the attributions to the case application of the landing gear taxiing simulation model.


References

[1] Civil Aviation Administration of China. Airworthiness standards for transport aircraft. CCAR-25-R4. 2011. http://www.caac.gov.cn/XXGK/XXGK/MHGZ/201606/t20160622_38638.html. Google Scholar

[2] Pritchard J. Overview of Landing Gear Dynamics. J Aircraft, 2001, 38: 130-137 CrossRef Google Scholar

[3] Krüger W R, Morandini M. Recent developments at the numerical simulation of landing gear dynamics. CEAS Aeronaut J, 2011, 1: 55-68 CrossRef Google Scholar

[4] Hajiloo A, Xie W F. Robust model predictive control of shimmy vibration in aircraft landing gears with probabilistic uncertainty. In: Proceedings of IEEE Conference on Control, 2014. 146--151. Google Scholar

[5] Besselink I J M. Shimmy of aircraft main landing gears. Dissertation for Ph.D. Degree. Delft: Delft University of Technology, 2000. Google Scholar

  • Figure 1

    (Color online) Taxiing stability simulation results. (a) Simulation model of NLG and MLG; (b) taxiing in symmetric scenario; (c) taxiing with lateral disturbance.

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