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一种Backstepping模型参考鲁棒飞行控制律的设计
引用本文:董文瀚,孙秀霞,林岩. 一种Backstepping模型参考鲁棒飞行控制律的设计[J]. 系统工程与电子技术, 2010, 32(7): 1485-1488. DOI: 10.3969/j.issn.1001506X.2010.07.031
作者姓名:董文瀚  孙秀霞  林岩
作者单位:(1. 空军工程大学工程学院, 陕西 西安 710038;;2. 北京航空航天大学自动化科学与电气工程学院, 北京 100191)
基金项目:国家自然科学基金,中国博士后科学基金 
摘    要:
提出了一种Backstepping模型参考鲁棒飞行控制律的设计方法。方法的主要特征是:在仅需要输入输出信号的情况下,即使系统参数未知且存在未建模动态和非线性因素干扰,系统仍能保证较强的鲁棒性,获得良好的跟踪效果。具体给出了飞机纵向通道短周期控制的设计方案,同时讨论了其他复杂模态下该方案的扩展方法。对上述方案的数值仿真显示了该方法良好的跟踪性能。

关 键 词:自适应控制  鲁棒控制  模型参考控制  飞行控制

Backstepping model reference robust controller design for flight control
DONG Wen-han,SUN Xiu-xia,LIN Yan. Backstepping model reference robust controller design for flight control[J]. System Engineering and Electronics, 2010, 32(7): 1485-1488. DOI: 10.3969/j.issn.1001506X.2010.07.031
Authors:DONG Wen-han  SUN Xiu-xia  LIN Yan
Affiliation:(1. Engineering Inst., Air Force Engineering Univ., Xi’an 710038, China; 2. School of Automation, Beihang Univ., Beijing 100191, China)
Abstract:
A Backstepping model reference robust control (MRRC) is used to solve the flight control problem. The main feature of the scheme is that only the plant input and output signals are needed and, even with the existence of plant uncertainty, unmodeled dynamics and non linear disturbance, both the tracking performance and the control effort can be improved significantly. The detailed design of longitudinal short period mode of an aircraft is given chiefly, and the design procedure for other modes whose relative degree is greater than one is discussed, too. The simulation results show that a perfect tracking performance can be achieved by using the design scheme.
Keywords:DONG Wen han  SUN Xiu xia   LIN Yan
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