Hangkong gongcheng jinzhan (Oct 2020)

Research on the Test Technology of Civil Aircraft Impacted by UAV Based on Rocket Sled

  • ZHENG Kuitao,
  • GONG Mingsheng,
  • JIANG Dapeng,
  • LIU Jun

DOI
https://doi.org/10.16615/j.cnki.1674-8190.2020.05.016
Journal volume & issue
Vol. 11, no. 5
pp. 724 – 729

Abstract

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The research on the damage degree of the key parts of civil aircraft impacted by UAV is a new hot issue in the field of civil aviation. It is the first time that rocket sled test is proposed to evaluate the safety of UAV colliding with civil aircraft. Through the research on collision speed, collision position, UAV attitude and parameter measurement, the technical scheme of collision is designed, and the design of rocket sled, trajectory control design, strength check and test scheme are discussed, and the test verification and simulation calculation are carried out. The results show that: the rocket sled collision test scheme designed in this paper is feasible, which can realize continuous multi-point collision on a single trajectory and record the whole process of multi angle, full coverage and high stability. It can provide the necessary technical reference for the subsequent similar collision tests, and the multiple impact tests also provide effective test data for the safety evaluation of UAV collision with civil aircraft.

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