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基于离散模糊滑模的飞行器角度跟踪控制
引用本文:曹立佳,颜诗源,张胜修,仇召辉.基于离散模糊滑模的飞行器角度跟踪控制[J].控制工程,2011,18(3):377-379,379.
作者姓名:曹立佳  颜诗源  张胜修  仇召辉
作者单位:1. 第二炮兵工程学院303室,陕西,西安,710025
2. 96604,部队,北京,100192
基金项目:国家自然科学基金资助项目(60874093)
摘    要:为解决某型飞行器的角度跟踪控制问题,设计了离散模糊滑模角度跟踪控制算法.以飞行器在空间的姿态运动方程为基础建立了其短周期运动模型.基于离散时间模糊滑模算法,设计了双入双出的模糊控制器,将滑模切换函数及其变化率作为模糊控制器的输入,以模糊控制器的二维输出信号为依据调整滑模趋近律的参数,该算法在减小了系统的抖振同时,保持了...

关 键 词:飞行器  角度跟踪  离散时间  模糊滑模控制

Aircraft Angle-Following Using Discrete-Time Fuzzy Sliding-Mode Control
CAO Li-jia,YAN Si-yuan,ZHANG Sheng-xiu,QIU Zhao-hui.Aircraft Angle-Following Using Discrete-Time Fuzzy Sliding-Mode Control[J].Control Engineering of China,2011,18(3):377-379,379.
Authors:CAO Li-jia  YAN Si-yuan  ZHANG Sheng-xiu  QIU Zhao-hui
Affiliation:CAO Li-jia1,YAN Si-yuan1,ZHANG Sheng-xiu1,QIU Zhao-hui2(1.The Second Artillery Engineering College,Xi'an 710025,China,2.96604 Team,Beijing,100192,China)
Abstract:Discrete-time fuzzy sliding-mode control algorithm is proposed to solve the problems of angle-following control for a specific aircraft.The model of short-period dynamics based on the attitude equations is given firstly.And the fuzzy controller for double-in-double-out is designed,in which switch function of sliding-mode and its change rate are used as the input of fuzzy-logic controller,output are used to regulate the approximation law of sliding-mode.This algorithm can reduce chattering of system and make...
Keywords:aircraft  angle-following  discrete-time  fuzzy sliding-mode control  
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