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Journal of Projectiles, Rockets, Missiles and Guidance >

2019 , Vol. 39 >Issue 4: 97 - 100

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.04.023

Study on Experimental Test of Aeroservoelasticity for Missiles

  • WANG Qishuang ,
  • LIU Junsheng ,
  • FU Bo ,
  • TAN Tianhan ,
  • YANG Yungang
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  • Xi'an Modern Control Technology Research Institute, Xi'an 710065, China

Received date: 2018-10-09

  Online published: 2025-05-19

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Abstract

Through the systematic reaserch of test theory of aeroservoelasticity, a experimental test method for missiles is proposed. Stability will be proved after the test, by choosing characteristic points of flight trajectory and doing a open-loop and close-loop experiment. The method is applied to a missile, and the coupling performance of the control system, structure and aerodynamics is tested, which guides the overall design of the missile and greatly improved the performance of the weapon.

Key words： aeroservoelasticity; control system; aerodynamics; stability; experimental test

Cite this article

WANG Qishuang , LIU Junsheng , FU Bo , TAN Tianhan , YANG Yungang . Study on Experimental Test of Aeroservoelasticity for Missiles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(4) : 97 -100 . DOI: 10.15892/j.cnki.djzdxb.2019.04.023

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