Adaptive tracking control of automatic net landing trajectory for carrier-based unmanned aerial vehicle

被引：0
|
作者：
Zhen Z. [1 ]
Tao G. [1 ,2 ]
Jiang J. [1 ]
Wang X. [1 ]
机构：
[1] College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] Department of Electrical and Computer Engineering, University of Virginia, Charlottesville
来源：
Zhen, Ziyang (zhenziyang@nuaa.edu.cn) | 1922年 / Editorial Board of Journal of Harbin Engineering卷 / 38期
关键词：
6-DOF; Adaptive control; Aerodynamic data; Automatic carrier landing; Flight control; Net landing trajectory; Nonlinear mathematical model; Trajectory tracking; Unmanned aerial vehicle;
D O I：
10.11990/jheu.201612061
中图分类号：
学科分类号：
摘要：
For a small carrier-based fixed-wing UAV, an automatic net landing technique was investigated. A 6-DOF nonlinear mathematical model of the UAV was established based on aerodynamic data. A guidance and control system structure was created for net landing of the UAV and a 3D reference glide path for net landing was designed. The filtering guide method was applied to design longitudinal and lateral guide laws. Adaptive control laws for elevator, throttle, aileron, and rudder control channels were separately designed by adopting the model reference adaptive control theory under the condition of unknown model parameters. Finally, the numerical simulation of a nonlinear carrier-based UAV was conducted. The results showed that the adaptive control method had precise performance in tracking landing trajectory. © 2017, Editorial Department of Journal of HEU. All right reserved.
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页码：1922 / 1927
页数：5
相关论文
共 10 条
  • [1] Naval interest in shipborne unmanned air vehicles, Naval Architect, pp. 45-46, (1997)
  • [2] Perry J.D., Navy unmanned air systems 1915-2011, Proceedings of AIAA Centennial of Naval Aviation Forum “100 Years of Achievement and Progress”, (2011)
  • [3] Yang Y., Carrier Landing Guidance and Control of Carrier-Based Aircraft, (2006)
  • [4] Zhen Z., Wang X., Jiang J., Et al., Research progress in guidance and control of automatic carrier landing of carrier-based aircraft, Acta aeronautica ET astronautica sinica, 38, 2, pp. 1-22, (2017)
  • [5] Yang Y., Zhen Z., Xu J., Et al., UAV Carrier Landing Guidance and Control, (2013)
  • [6] Li R., Zhen Z., Gong H., Trajectory control of a UAV during net recovery based on sliding mode control and optimal control, Electronics Optics and Control, 21, 9, (2014)
  • [7] Zheng F.Y., Gong H.J., Zhen Z.Y., Adaptive constraint backstepping fault tolerant control for small carrier UAV with uncertain parameters, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 230, pp. 407-425, (2016)
  • [8] Zheng F.Y., Zhen Z.Y., Gong H.J., Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults, Journal of Systems Engineering and Electronics, 28, 2, pp. 322-337, (2017)
  • [9] Tao G., Adaptive Control Design and Analysis, (2003)
  • [10] Goodwin G.C., Graebe S.F., Salgado M.E., Control System Design, (2001)
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