Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface
Airplane control system is a typical multitude input and multitude output (MIMO) nonlinear system with strong coupling and uncertainties, which would increase the controlling difficulty. The tracking control problem has been investigated for a class of airplane attitude control systems in this paper...
Main Authors: | , , , |
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Format: | Article |
Language: | zho |
Published: |
Hebei University of Science and Technology
2018-10-01
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Series: | Journal of Hebei University of Science and Technology |
Subjects: | |
Online Access: | http://xuebao.hebust.edu.cn/hbkjdx/ch/reader/create_pdf.aspx?file_no=b201805008&flag=1&journal_ |