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弹箭与制导学报 >

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

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

导弹与制导技术

基于 PID 控制对伸缩翼飞行器变形时间的研究

  • 苏浩秦 ,
  • 包晓翔 ,
  • 李新华 ,
  • 李平坤 ,
  • 曾立科 ,
  • 刘凯
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  • 中国航天空气动力技术研究院第11部,北京 100074

苏浩秦(1975-),男,陕西西安人,高级工程师,博士,研究方向:飞行器总体设计与控制。

包晓翔,男,.

收稿日期: 2014-03-26

  网络出版日期: 2025-05-26

基金资助

总装2012年技术基础计划(HK30120121BZ39)

收起

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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摘要

伸缩翼飞行器随着飞行任务变化而相应的改变其外形,始终保持最优飞行状态,以达到在复杂飞行环境中执行多种任务的要求。文中首先建立伸缩翼无人机运动模型和变形过程的气动模型,随后采用根轨迹方法设计PID控制器,实现对飞行器的纵向控制,最后采用仿真方法研究飞行器伸缩翼的变形过程,通过对比选择最佳伸缩变形时间。

关键词： 变形飞行器; 伸缩翼; PID控制; 变形时间

本文引用格式

苏浩秦 , 包晓翔 , 李新华 , 李平坤 , 曾立科 , 刘凯 . 基于 PID 控制对伸缩翼飞行器变形时间的研究[J]. 弹箭与制导学报, 2015 , 35(2) : 10 -12,16 . DOI: 10.15892/j.cnki.djzdxb.2015.02.003

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

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参考文献

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