Design of aircraft optimal time-delay feedback controller

被引：0
|
作者：
Meng, Xin-Yu [1 ,2 ]
Wang, Dao-Bo [1 ]
Tang, Xiao-Jun [1 ]
Yang, Jian-Dong [3 ]
机构：
[1] College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] Northwest Institute of Nuclear Technology, Xi'an
[3] China Satellite Maritime Tracking and Control Center, Jiangyin
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2014年 / 36卷 / 11期
关键词：
Aircraft; Optimal control; State transformation; Time-delay;
D O I：
10.3969/j.issn.1001-506X.2014.11.23
中图分类号：
学科分类号：
摘要：
Since a system has a characteristic of control delay during the design of the aircraft optimal feedback controller, the delay control system is transformed to a non-delay control system by utilizing the continuous states transform method. Then using the solution of the non-delay control system, which makes the performance index smallest, the state function of the original system can be calculated. With the help of relationship between the delay feedback control and the state-transformed optimal control, it can help find the gain of the optimal time-delay feedback control. Simulation is made to verify the hovering data of unmanned helicopter experiments and the results validate the proposed control method. ©, 2014, Chinese Institute of Electronics. All right reserved.
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页码：2255 / 2258
页数：3
相关论文
共 14 条
  • [1] Nair V.G., George V.I., Prahlad K.R., Lateral contral of aircraft, considering the cross-coupling effect of yaw and roll on each-other using fuzzy logic, Sensors and Transducers, 142, 7, pp. 105-117, (2012)
  • [2] Liu Y., Tao G., Joshi S.M., Modeling and model reference adaptive control of aircraft with asymmetric damage, Journal of Guidance, Control, and Dynamics, 33, 5, pp. 1500-1517, (2010)
  • [3] Balakrishnan S.N., Biega V., Adaptive-critic-based neural networks for aircraft optimal control, Journal of Guidance, Control, and Dynamics, 19, 4, pp. 893-898, (1996)
  • [4] Akpan V.A., Hassapis G.D., Nonlinear model identification and adaptive model predictive control using neural networks, ISA Transactions, 50, 2, pp. 177-194, (2011)
  • [5] Huang C.S., Yuan K., Output tracking of a non-linear non-minimum phase PVTOL aircraft based on non-linear state feedback control, International Journal of Control, 75, 6, pp. 466-473, (2002)
  • [6] Tang G.Y., Li J., Optimal fault diagnosis for systems with delayed measurements, IET Control Theory and Applications, 2, 11, pp. 990-998, (2008)
  • [7] Li J., Ye R.H., Fault diagnosis and dynamic optimal fault-tolerant control for systems with double time-delays, Control Theory and Applications, 25, 6, pp. 1021-1026, (2008)
  • [8] Lin Y.C., Lin C.L., Optimal control approach for robust control design of neutral systems, Optimal Control Applications and Methods, 30, 1, pp. 87-102, (2009)
  • [9] Haratishvili G.L., A Maximum Principle in External Problems with Delays in Mathematical Theory of Control, (1967)
  • [10] Tang G.Y., Wang H.H., Suboptimal control for discrete linear systems with time-delay: A successive approximation approach , Acta Automatica Sinic, 31, 3, pp. 419-426, (2005)
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