DocumentCode
2081324
Title
To reduce initial control magnitude in backstepping: A continuous predictive approach
Author
Hou, Mingzhe ; Duan, Guangren ; Liang, Xiaoling ; Deng, Zongquan
Author_Institution
Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, Heilongjiang Province, China 150001
fYear
2015
fDate
May 31 2015-June 3 2015
Firstpage
1
Lastpage
6
Abstract
In this paper, a novel backstepping control algorithm is proposed by adopting the nonlinear continuous predictive approach. An optimization performance index containing the weighted tracking error and control input is introduced to obtain the actual control law. By adjusting the weighting matrix, the control magnitude in the initial stage can be reduced. In addition, when the weighting matrix imposing on input vector vanishes, the control law just coincides with the traditional backstepping control law. The proposed approach is further applied to the control of aircrafts. The simulation results show the effectiveness and advantage of our method.
Keywords
Aerospace control; Aircraft; Backstepping; Closed loop systems; Nonlinear systems; Optimization; Performance analysis; aircraft control; backstepping control; continuous predictive approach; control magnitude;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ASCC), 2015 10th Asian
Conference_Location
Kota Kinabalu, Malaysia
Type
conf
DOI
10.1109/ASCC.2015.7244374
Filename
7244374
Link To Document