SMOOTH SWITCHING OUTPUT TRACKING CONTROL FOR LPV SYSTEMS

被引:14
|
作者
Song, Lei [1 ]
Yang, Jianying [2 ,3 ]
机构
[1] Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China
[2] Peking Univ, Coll Engn, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China
[3] Peking Univ, Coll Engn, Dept Mech & Aerosp Engn, Beijing 100871, Peoples R China
关键词
Output tracking control; smooth switching; LPV systems; LMI; H-INFINITY CONTROL; FLIGHT-CONTROL; GAIN;
D O I
10.1002/asjc.510
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper is concerned with the problem of smooth switching state feedback controller design for aircraft dynamic systems with multiple operating points. Based on the theory of robust control, a single state feedback controller which considers smooth switching is constructed. With the constant controller, the output response can be considerably improved in the switching process when the flight condition changes. An example for autopilot design of an F-18 aircraft is given to illustrate the effectiveness of the proposed approach.
引用
收藏
页码:1710 / 1716
页数:7
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