Study of Variable Structure Control Technology on Stratospheric Airship Attitude

摘要：

Aim at autonomous control of stratosphere airship, the paper addresses one attitude controller design approach based on the small disturbance model of airship. The controller was designed based on the theory of output feedback variable structure control, the variable plane is designed by solving a set of bilinear matrix inequality transformation and a set of linear matrix inequalities iterative. Base on high improved gain method, it availably reduce shake used to adding a little and positive quantization in the denominator of control law. Then the control system made up of output feedback variable structure controller is simulated, the simulation results show that this method has excellent control effect.

关键词： attitude control small disturbance model variable structure controller linear matrix inequalities

作者: Linlin HE Wenli HUANG Yanfang WANG

作者单位: School of Mechatronics Engineering Zhengzhou institute of Aeronautical Industry Management Zhengzhou, China

会议类型: 国际会议

会议名称: 2012 International Conference on Measurement,Information and Control(2012测量、信息与控制国际会议 ICMIC2012)

会议地点: 哈尔滨

会议语种:英文

页码: 1015-1018

在线出版日期: 2012-05-18（万方平台首次上网日期，不代表论文的发表时间）