摘要
介绍了模糊控制技术的基本原理和设计方法,应用带修正因子的模糊控制技术设计了飞行器姿态控制系统,并进行了数学仿真。结果表明,该方法可以快速消除姿态角偏差,克服各种随机干扰,姿态角具有良好的动态响应特性。
The principle and the design method of fuzzy logic control （FLC） technology are introduced in this paper. The attitude control system for aerocraft by using FLC with mend coefficient and digital simulation is designed. The simulation results show that the method can eliminate attitude deviation and overcome disturbance of diverse kinds. The attitude of missile has favorable dynamic properties.
出处
《航天控制》
CSCD
北大核心
2013年第2期28-32,共5页
Aerospace Control
关键词
模糊控制
姿态控制
隶属函数
修正因子
Fuzzy logic control
Attitude control
Attitude angle deviation
