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 :
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