High AOA decoupling control for aircraft based on ADRC

doi:10.23919/JSEE.2020.000016

Journal of Systems Engineering and Electronics ›› 2020, Vol. 31 ›› Issue (2): 393-402.doi: 10.23919/JSEE.2020.000016

• Control Theory and Application • Previous Articles Next Articles

High AOA decoupling control for aircraft based on ADRC

Junjie LIU(), Mingwei SUN(), Zengqiang CHEN*(), Qinglin SUN()

College of Artificial Intelligence, Nankai University, Tianjin 300350, China

Received:2019-05-20 Online:2020-04-30 Published:2020-04-30
Contact: Zengqiang CHEN E-mail:ljjtju@163.com;sunmingwei@163.com;chenzq@nankai.edu.cn;sunql@nankai.edu.cn
About author:LIU Junjie was born in 1991. He received his M.S. degree in control science and engineering from Tianjin University of Technology. Currently, he is pursuing his Ph.D. degree in the College of Artificial Intelligence, Nankai University. His research interests include active disturbance rejection control and flight control. E-mail: ljjtju@163.com|SUN Mingwei was born in 1972. He received his Ph.D. degree in control science and engineering, Nankai University. Now he is a professor in the College of Artificial Intelligence, Nankai University. His research interests include active disturbance rejection control, nonlinear control, flight control, guidance and optimization. E-mail: smw sunmingwei@163.com|CHEN Zengqiang was born in 1964. He received his Ph.D. degree in control science and engineering, Nankai University. Now he is a professor in the College of Artificial Intelligence, Nankai University. His research interests include predictive control, active disturbance rejection control and nonlinear control. E-mail: chenzq@nankai.edu.cn|SUN Qinglin was born in 1964. He received his Ph.D. degree in control science and engineering, Nankai University. Now he is a professor in the College of Artificial Intelligence, Nankai University. His research interests include parafoil control, active disturbance rejection control and nonlinear control. E-mail: sunql@nankai.edu.cn
Supported by:
the National Natural Science Foundation of China(61973175);the National Natural Science Foundation of China(61973172);This work was supported by the National Natural Science Foundation of China (61973175; 61973172)

Abstract

Abstract:

In this paper, a practical decoupling control scheme for fighter aircraft is proposed to achieve high angle of attack (AOA) tracking and super maneuver action by utilizing the thrust vector technology. Firstly, a six degree-of-freedom (DOF) nonlinear model with 12 variables is given. Due to low sufficiency of the aerodynamic actuators at high AOA, a thrust vector model with rotatable engine nozzles is derived. Secondly, the active disturbance rejection control (ADRC) is used to realize a three-channel decoupling control such that a strong coupling between different channels can be treated as total disturbance, which is estimated by the designed extended state observer. The control surface allocation is implemented by the traditional daisy chain method. Finally, the effectiveness of the presented control strategy is demonstrated by some numerical simulation results.

Key words: high angle of attack (AOA), decoupling control, linear extended state observer (LESO), active disturbance rejection control (ADRC), thrust vector technology, control allocation

Junjie LIU, Mingwei SUN, Zengqiang CHEN, Qinglin SUN. High AOA decoupling control for aircraft based on ADRC[J]. Journal of Systems Engineering and Electronics, 2020, 31(2): 393-402.

Figures/Tables 8

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Control surface	Bandwidth /(rad/s)	Rate /(°/s)	Position /(°)
Aileron	20.2	±80	±21.5
Elevator	20.2	±80	±25
Rudder	20.2	±120	±30
Roll	30.2	±150	±20
Yaw	30.2	±150	±20
Pitch	30.2	±150	±20

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[3]	Yueyue Ma, Jie Guo, and Shengjing Tang. BTT autopilot design for agile missiles with aerodynamic uncertainty [J]. Journal of Systems Engineering and Electronics, 2015, 26(4): 802-.
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High AOA decoupling control for aircraft based on ADRC

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