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Taxiing stability verification and airworthiness certification for amphibious aircraft

  • Xufei HeEmail author
  • Jianliang Ai
Letter
  • 11 Downloads

Notes

Acknowledgements

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

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    Civil Aviation Administration of China. Airworthiness standards for transport aircraft. CCAR-25-R4. 2011. https://doi.org/www.caac.gov.cn/XXGK/XXGK/MHGZ/201606/t20160622_38638.html
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    Krüger W R, Morandini M. Recent developments at the numerical simulation of landing gear dynamics. CEAS Aeronaut J, 2011, 1: 55–68CrossRefGoogle Scholar
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    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. 146–151Google Scholar
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    Besselink I J M. Shimmy of aircraft main landing gears. Dissertation for Ph.D. Degree. Delft: Delft University of Technology, 2000Google Scholar

Copyright information

© Science China Press and Springer-Verlag GmbH Germany, part of Springer Nature 2018

Authors and Affiliations

  1. 1.Department of AerospaceFudan UniversityShanghaiChina
  2. 2.Shanghai Aircraft Airworthiness Certification Center of CAACShanghaiChina

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