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飞机增稳系统的耗散控制问题研究
引用本文:张旸,唐海峰,马永强.飞机增稳系统的耗散控制问题研究[J].飞机设计,2013(5):44-46.
作者姓名:张旸  唐海峰  马永强
作者单位:[1]海军驻沈阳地区航空军事代表室,辽宁沈阳110034 [2]沈阳桃仙国际机场股份有限公司信息机电中心技培室,辽宁沈阳110169
摘    要:讨论了飞机增稳系统的耗散控制问题.首先将增稳系统的运动方程简化为定常线性系统;其次,研究系统的耗散性分析;再次,设计状态反馈控制器使得系统的闭环系统耗散;最后,通过数值仿真验证了方法的可行性。

关 键 词:增急系统  耗散  状态反馈控制器

Study on Dissipative Control for an Aircraft Augmentation System
ZHANG Yang,TANG Hai-feng,MA Yong-qiang.Study on Dissipative Control for an Aircraft Augmentation System[J].Aircraft Design,2013(5):44-46.
Authors:ZHANG Yang  TANG Hai-feng  MA Yong-qiang
Institution:1. PLA Navy Military Consumer Representative Office in Shenyang, Shenyang 110034, China) (2. Technically Training Office of Mechanicaland Electronic Information Certer, Shenyang Taoxian International Airport Co., Ltd. Shenyang 110169, China )
Abstract:Dissipative control problem for an aircraft augmentation system is discussed in the paper. Firstly, the dynamical equation of augmentation system is reduced to a linear time-invariant system; secondly, the dissipation of the system is discussed; thirdly, the state feedback controller to make the closed-loop system be dissipative; at last, we testify the feasibility of the method by a numerical example.
Keywords:augmentation system  dissipative  state feedback controler
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