• CN: 11-2187/TH
  • ISSN: 0577-6686

Journal of Mechanical Engineering ›› 2022, Vol. 58 ›› Issue (15): 216-225.doi: 10.3901/JME.2022.15.216

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Research on the Calculation Method of the Success Rate of Carrier-Based Aircraft Landing and Hooking Cable

PENG Yiming1,2, YIN Yin2, WEI Xiaohui1,2, NIE Hong1,2   

  1. 1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016;
    2. Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016
  • Received:2021-09-13 Revised:2022-03-20 Online:2022-08-05 Published:2022-10-13

Abstract: The arresting process of carrier-based aircraft landing is a complex and dangerous process, which includes many uncertain factors, so it is difficult to analyze the reliability of landing arresting.In order to make the analysis of the landing arresting reliability more accurate and effective, a certain type of carrier-based aircraft is taken as the research object, establishes a dynamic model of the aircraft landing and hooking cable, and verifies the accuracy of the model through the dynamic test results.Then perform batch simulation on the dynamic model to obtain the sample points needed to establish the proxy model.Finally, the proxy model of the reliability of the arresting hook hooking cable is established by using the support vector machine method, and the Monte Carlo method is used to analyze the reliability of the landing and hooking cable, and the success rate of hooking cable is calculated.The analysis method and its results can provide reference for the design of the top-level parameters of the carrier-based aircraft and the reliability research of the arresting system.

Key words: carrier-based aircraft, arrest, dynamic, proxy model, reliability

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