Robust adaptive attitude control for carrier based aircrafts in the landing process under the carrier air wake disturbance
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- 英文论文题名：Robust adaptive attitude control for carrier based aircrafts in the landing process under the carrier air wake disturbance
- 论文作者：Jianglong Yu ; Yongzhao Hua ; Peng Yang ; Xiwang Dong ; Qingdong Li ; Zhang Ren
- 英文论文作者：Jianglong Yu ; Yongzhao Hua ; Peng Yang ; Xiwang Dong ; Qingdong Li ; Zhang Ren ; School of Automation Science and Electrical Engineering ; Science and Technology on Aircraft Control Laboratory ; Beihang University ; Aviation System Research Department ; System Engineering Research Institute
- 年：2017
- 作者机构：School of Automation Science and Electrical Engineering,Science and Technology on Aircraft Control Laboratory,Beihang University;Aviation System Research Department,System Engineering Research Institute;
- 英文论文关键词：Carrier based aircraft ; Carrier air wake ; Disturbance ; Robust adaptive control ; Nonlinear extended state observer
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（B）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
- 语种：英文
- 分类号：V249.121
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：6
- 文件大小：268k
- 原文格式：D
- 会议级别：全国
摘要
When naval vessels moving on the sea, the carrier air wake disturbance will arise. The carrier air wake makes the landing environment of carrier aircraft fair adverse, which puts forward a high demand for the high precise attitude control of carrier based aircrafts. In this paper, high precise robust attitude control problems for carrier based aircrafts with the carrier air wake disturbance are investigated. Firstly, the small disturbance linearization method is introduced to transform the nonlinear system into a linear one, which is a necessary procedure for aircraft system analysis and controller design. Secondly, the model of the carrier air wake disturbance is established and its effects on the aerodynamic parameters are analyzed in detail. Then the effects are transformed into the augmented disturbance in the system. Thirdly, a nonlinear extended state observer is utilized to estimate the disturbance. Besides, a robust adaptive attitude controller with integral term is proposed to achieve high precision attitude tracking. The stability of the closed-loop system is prove based on Lyapunov theory. Finally, a numerical example is provided to demonstrate the effectiveness of the obtained results.
When naval vessels moving on the sea, the carrier air wake disturbance will arise. The carrier air wake makes the landing environment of carrier aircraft fair adverse, which puts forward a high demand for the high precise attitude control of carrier based aircrafts. In this paper, high precise robust attitude control problems for carrier based aircrafts with the carrier air wake disturbance are investigated. Firstly, the small disturbance linearization method is introduced to transform the nonlinear system into a linear one, which is a necessary procedure for aircraft system analysis and controller design. Secondly, the model of the carrier air wake disturbance is established and its effects on the aerodynamic parameters are analyzed in detail. Then the effects are transformed into the augmented disturbance in the system. Thirdly, a nonlinear extended state observer is utilized to estimate the disturbance. Besides, a robust adaptive attitude controller with integral term is proposed to achieve high precision attitude tracking. The stability of the closed-loop system is prove based on Lyapunov theory. Finally, a numerical example is provided to demonstrate the effectiveness of the obtained results.
When naval vessels moving on the sea, the carrier air wake disturbance will arise. The carrier air wake makes the landing environment of carrier aircraft fair adverse, which puts forward a high demand for the high precise attitude control of carrier based aircrafts. In this paper, high precise robust attitude control problems for carrier based aircrafts with the carrier air wake disturbance are investigated. Firstly, the small disturbance linearization method is introduced to transform the nonlinear system into a linear one, which is a necessary procedure for aircraft system analysis and controller design. Secondly, the model of the carrier air wake disturbance is established and its effects on the aerodynamic parameters are analyzed in detail. Then the effects are transformed into the augmented disturbance in the system. Thirdly, a nonlinear extended state observer is utilized to estimate the disturbance. Besides, a robust adaptive attitude controller with integral term is proposed to achieve high precision attitude tracking. The stability of the closed-loop system is prove based on Lyapunov theory. Finally, a numerical example is provided to demonstrate the effectiveness of the obtained results.
引文
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[2]M.Steinberg,Development and simulation of an F/A-18 fuzzy logic automatic carrier landing system,in Proceedings of IEEE Second IEEE International Conference on Fuzzy Systems,797–802,1993.
[3]J.Crassidis J and D.Mook,Robust control design of an automatic carrier landing system,in Proceedings of Astrodynamics Conference 1417–1481,1992.
[4]M.B.Subrahmanyam,H∞design of F/A-18A automatic Carrier Landing System,Journal of guidance,control,and dynamics,17(1):187-191,1994.
[5]A.Page A and M.Steinberg,A comparison of neural,fuzzy,evolutionary,and adaptive approaches for carrier landing,in Proceedings of AIAA Guidance,Navigation,and Control Conference and Exhibit,1-11,2001.
[6]J.Chen,W,Han,and G.Xu,Carrier landing flight path angle control via higher-order sliding mode.in Proceedings of IEEE Sixth International Conference on Intelligent Human-Machine Systems and Cybernetics,2:146-149,2014.
[7]Y.Yu,H.L.Wang,X.L.Shao,and H.Yu,The attitude control of UAV in carrier landing based on ADRC,in Proceedings of IEEE Chinese Guidance,Navigation and Control Conference,832-837,2016.
[8]J.Li and H.B.Duan,Simplified brain storm optimization approach to control parameter optimization in F/A-18 automatic carrier landing system,Aerospace Science and Technology,42:187-195,2015.
[9]Y.Deng and H.B.Duan,Control parameter design for automatic carrier landing system via pigeon-inspired optimization,Nonlinear Dynamics,85(1):97-106,2016.
[10]L.P.Wang,Q.D.Zhu,Z.Zhang,and R.Dong,Modeling pilot behaviors based on discrete-time series during carrier-based aircraft landing,Journal of Aircraft,53(6):1922–1931,2016.
[11]Q.H.Shi,Study on the control technology for carrier aircraft landing,Harbin Engineering University,2006.
[12]M.Cui,Design on flight guidance and control system of automatic carrier landing,Harbin Engineering University,2013.
[13]L.Shi,Analysis of the influence of the disturbance on the landing of the carrier based aircraft,Shanghai Jiao Tong University,2009.
[14]G.H.Xia,R.Dong,J.T.Xu,and Q.D.Zhu,Linearized model of carrier based aircraft dynamics in final approach air condition,Journal of Aircraft,53(1):1-15,2015.
[15]M.Green and D.J.N Limebeer,Linear robust control.Prentice-Hall:Inc,1994.
[16]Z.X.Li,Y.J.He,G.C.Zhang,J.Q.Li,and Y.Zhang,Calculation of the additional attack angle and the additional sideslip angle of craft caused by wind disturbance,Missiles and space vehicles,(5):66-73,2016.
[17]Y.Huang and J.Q.Han,Analysis and design of nonlinear continuous second order extended state observer,Chinese Science Bulletin,45(13):1373-1379,2000.
[18]Li.Gao,W.H.Wu,D.Mei,and Z.G.Qu,Design and Simulation of Automatic Carrier Landing Control System,Ordnance Industry Automation,35(3):86-89,2016.
[2]M.Steinberg,Development and simulation of an F/A-18 fuzzy logic automatic carrier landing system,in Proceedings of IEEE Second IEEE International Conference on Fuzzy Systems,797–802,1993.
[3]J.Crassidis J and D.Mook,Robust control design of an automatic carrier landing system,in Proceedings of Astrodynamics Conference 1417–1481,1992.
[4]M.B.Subrahmanyam,H∞design of F/A-18A automatic Carrier Landing System,Journal of guidance,control,and dynamics,17(1):187-191,1994.
[5]A.Page A and M.Steinberg,A comparison of neural,fuzzy,evolutionary,and adaptive approaches for carrier landing,in Proceedings of AIAA Guidance,Navigation,and Control Conference and Exhibit,1-11,2001.
[6]J.Chen,W,Han,and G.Xu,Carrier landing flight path angle control via higher-order sliding mode.in Proceedings of IEEE Sixth International Conference on Intelligent Human-Machine Systems and Cybernetics,2:146-149,2014.
[7]Y.Yu,H.L.Wang,X.L.Shao,and H.Yu,The attitude control of UAV in carrier landing based on ADRC,in Proceedings of IEEE Chinese Guidance,Navigation and Control Conference,832-837,2016.
[8]J.Li and H.B.Duan,Simplified brain storm optimization approach to control parameter optimization in F/A-18 automatic carrier landing system,Aerospace Science and Technology,42:187-195,2015.
[9]Y.Deng and H.B.Duan,Control parameter design for automatic carrier landing system via pigeon-inspired optimization,Nonlinear Dynamics,85(1):97-106,2016.
[10]L.P.Wang,Q.D.Zhu,Z.Zhang,and R.Dong,Modeling pilot behaviors based on discrete-time series during carrier-based aircraft landing,Journal of Aircraft,53(6):1922–1931,2016.
[11]Q.H.Shi,Study on the control technology for carrier aircraft landing,Harbin Engineering University,2006.
[12]M.Cui,Design on flight guidance and control system of automatic carrier landing,Harbin Engineering University,2013.
[13]L.Shi,Analysis of the influence of the disturbance on the landing of the carrier based aircraft,Shanghai Jiao Tong University,2009.
[14]G.H.Xia,R.Dong,J.T.Xu,and Q.D.Zhu,Linearized model of carrier based aircraft dynamics in final approach air condition,Journal of Aircraft,53(1):1-15,2015.
[15]M.Green and D.J.N Limebeer,Linear robust control.Prentice-Hall:Inc,1994.
[16]Z.X.Li,Y.J.He,G.C.Zhang,J.Q.Li,and Y.Zhang,Calculation of the additional attack angle and the additional sideslip angle of craft caused by wind disturbance,Missiles and space vehicles,(5):66-73,2016.
[17]Y.Huang and J.Q.Han,Analysis and design of nonlinear continuous second order extended state observer,Chinese Science Bulletin,45(13):1373-1379,2000.
[18]Li.Gao,W.H.Wu,D.Mei,and Z.G.Qu,Design and Simulation of Automatic Carrier Landing Control System,Ordnance Industry Automation,35(3):86-89,2016.