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...
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| Format: | Article |
| Language: | zho |
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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_ |
| _version_ | 1818952056541544448 |
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| author | Xiaojing WU Xueli WU Shikai SHAO Huixian LIU |
| author_facet | Xiaojing WU Xueli WU Shikai SHAO Huixian LIU |
| author_sort | Xiaojing WU |
| collection | DOAJ |
| description | 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. Firstly, a new higher-order differential sliding mode surface is presented and its stability of the sliding mode surface is proved by coordinate transformation of airplane attitude control system and considering the existing of the input uncertainties. Then, a smooth adaptive sliding mode controller is design based on this higher-order differential sliding mode surface and the approximation ability of the neural network. Based on Lyapunov stability theory, it is proved that the designed controller not only ensures the airplane attitude control system with good tracking performance, but also avoids the appearance of the chattering phenomenon of traditional sliding mode controllers. Finally, the effectiveness of the proposed controller is verified by simulation results. The controller proposed in this paper has very fine application prospects in the field of airplane attitude control comparing the traditional one. |
| first_indexed | 2024-12-20T09:44:19Z |
| format | Article |
| id | doaj.art-bd8c10d90b3245fd8d1121014792c69b |
| institution | Directory Open Access Journal |
| issn | 1008-1542 |
| language | zho |
| last_indexed | 2024-12-20T09:44:19Z |
| publishDate | 2018-10-01 |
| publisher | Hebei University of Science and Technology |
| record_format | Article |
| series | Journal of Hebei University of Science and Technology |
| spelling | doaj.art-bd8c10d90b3245fd8d1121014792c69b2022-12-21T19:44:47ZzhoHebei University of Science and TechnologyJournal of Hebei University of Science and Technology1008-15422018-10-0139543043710.7535/hbkd.2018yx05008b201805008Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surfaceXiaojing WU0Xueli WU1Shikai SHAO2Huixian LIU3School of Electrical Engineering, Hebei University of Science and Technology, Shijiazhuang, Hebei 050018, ChinaSchool of Electrical Engineering, Hebei University of Science and Technology, Shijiazhuang, Hebei 050018, ChinaSchool of Electrical Engineering, Hebei University of Science and Technology, Shijiazhuang, Hebei 050018, ChinaSchool of Electrical Engineering, Hebei University of Science and Technology, Shijiazhuang, Hebei 050018, ChinaAirplane 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. Firstly, a new higher-order differential sliding mode surface is presented and its stability of the sliding mode surface is proved by coordinate transformation of airplane attitude control system and considering the existing of the input uncertainties. Then, a smooth adaptive sliding mode controller is design based on this higher-order differential sliding mode surface and the approximation ability of the neural network. Based on Lyapunov stability theory, it is proved that the designed controller not only ensures the airplane attitude control system with good tracking performance, but also avoids the appearance of the chattering phenomenon of traditional sliding mode controllers. Finally, the effectiveness of the proposed controller is verified by simulation results. The controller proposed in this paper has very fine application prospects in the field of airplane attitude control comparing the traditional one.http://xuebao.hebust.edu.cn/hbkjdx/ch/reader/create_pdf.aspx?file_no=b201805008&flag=1&journal_cyberneticsairplane attitude controladaptive sliding mode controlsliding mode surfaceuncertainty |
| spellingShingle | Xiaojing WU Xueli WU Shikai SHAO Huixian LIU Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface Journal of Hebei University of Science and Technology cybernetics airplane attitude control adaptive sliding mode control sliding mode surface uncertainty |
| title | Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface |
| title_full | Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface |
| title_fullStr | Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface |
| title_full_unstemmed | Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface |
| title_short | Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface |
| title_sort | adaptive sliding mode control for uncertain airplane control systems based on higher order differential sliding mode surface |
| topic | cybernetics airplane attitude control adaptive sliding mode control sliding mode surface uncertainty |
| url | http://xuebao.hebust.edu.cn/hbkjdx/ch/reader/create_pdf.aspx?file_no=b201805008&flag=1&journal_ |
| work_keys_str_mv | AT xiaojingwu adaptiveslidingmodecontrolforuncertainairplanecontrolsystemsbasedonhigherorderdifferentialslidingmodesurface AT xueliwu adaptiveslidingmodecontrolforuncertainairplanecontrolsystemsbasedonhigherorderdifferentialslidingmodesurface AT shikaishao adaptiveslidingmodecontrolforuncertainairplanecontrolsystemsbasedonhigherorderdifferentialslidingmodesurface AT huixianliu adaptiveslidingmodecontrolforuncertainairplanecontrolsystemsbasedonhigherorderdifferentialslidingmodesurface |