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Journal of Projectiles, Rockets, Missiles and Guidance >

2015 , Vol. 35 >Issue 2: 10 - 12,16

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.02.003

MISSILES AND GUIDANCE TECHNOLOGY

Morphing Time Research for Flexing Wing Aircraft Based on PID Controller

  • SU Haoqin ,
  • BAO Xiaoxiang ,
  • LI Xinhua ,
  • LI Pingkun ,
  • ZENG Like ,
  • LIU Kai
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  • The 11th Department of China Academy of Aerospace Aerodynamic, Beijing 100074, China

Received date: 2014-03-26

  Online published: 2025-05-26

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Abstract

Morphing aircraft changes its profile to fit the varied flight tasks, and the optimal states are kept to complete requirement of task under complex conditions. In this paper, firstly, the kinematic model and morphing aerodynamic model of morphing aircraft were built, then longitudinal control of aircraft can be realized by PID controller, at last, flexing wing process was researched by simulation, and the best morphing time can be selected.

Key words： morphing aircraft; flexing wing; PID controller; morphing time

Cite this article

SU Haoqin , BAO Xiaoxiang , LI Xinhua , LI Pingkun , ZENG Like , LIU Kai . Morphing Time Research for Flexing Wing Aircraft Based on PID Controller[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(2) : 10 -12,16 . DOI: 10.15892/j.cnki.djzdxb.2015.02.003

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