Adaptive radial basis function neural network control of a wire-driven parallel robot based on local model approximation

被引:0
|
作者
Wang Y.-Q. [1 ]
Lin Q. [2 ]
Zhou L. [1 ]
Shi X.-X. [1 ]
Du Y.-J. [1 ]
Qiao G.-F. [1 ]
机构
[1] School of Automation, Nanjing Institute of Technology, Nanjing
[2] School of Aerospace Engineering, Xiamen University, Xiamen
来源
Wang, Yu-Qi (940898628@qq.com) | 1600年 / South China University of Technology卷 / 38期
基金
中国国家自然科学基金;
关键词
Adaptive control; Local model approximation; Lyapunov function; RBF neural network; Wire-driven parallel robot;
D O I
10.7641/CTA.2020.00184
中图分类号
学科分类号
摘要
In order to ensure the pose of the end effector of wind tunnel test wire-driven parallel robot (WTT-WDPR), an adaptive RBF neural network control based on local model approximation is proposed. The dynamic equation of the aircraft model is established by Newton Euler method, and the dynamic equation of the driving system is established based on the dynamic moment balance equation. In this paper, RBF neural network is used to design the approximation of local model and control law, and Lyapunov function is constructed to analyze the stability of the system. The results show that WTT-WDPR tends to be asymptotically stable. The WTT-WDPR is simulated by MATLAB/Simulink. The simulation results verify the correctness and feasibility of the designed adaptive RBF neural network control, meet the requirements of system control accuracy, and lay a theoretical foundation for practical application and technical realization on the prototype. © 2021, Editorial Department of Control Theory & Applications South China University of Technology. All right reserved.
引用
收藏
页码:380 / 390
页数:10
相关论文
共 24 条
  • [1] MELBER-WILKENDING S, HEIDEBRECHT A, WICHMANN G., A new approach in CFD supported wind tunnel testing, The 25th International Congress of the Aeronautical Sciences, pp. 1-10, (2006)
  • [2] WANG Xiaoguang, LIN Qi, Progress in wire-driven parallel suspension technologies in wind tunnel tests, Acta Aeronautica et Astronautica Sinica, 39, 10, pp. 1-20, (2018)
  • [3] LAFOURCADE P, LLIBRE M, REBOULET C., Design of a parallel wire-driven manipulator for wind tunnels, Proceedings of the Workshop on Fundamental Issues and Future Research Directions for Parallel Mechanisms and Manipulators, pp. 187-194, (2002)
  • [4] LAFOURCADE P, LLIBRE M., First steps toward a sketch-based design methodology for wire-driven manipulators, IEEE/ASME International Conference on Advanced Intelligent Mechatronics, pp. 143-148, (2003)
  • [5] LAFOURCADE P., Study of parallel manipulators with cables, design of an active suspension for wind tunnel, (2004)
  • [6] LAMBERT T J, VUKASINOVIC B, GLEZER A., A six degrees of freedom dynamic wire-driven traverse, Aerospace, 3, 2, pp. 1-16, (2016)
  • [7] LAMBERT T J., Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body, (2016)
  • [8] LAMBERT T J, VUKASINOVIC B, GLEZER A., Aero-dynamic flow control of wake dynamics coupled to a moving bluff body, The 8th AIAA Flow Control Conference, pp. xx-xx, (2016)
  • [9] BRUCKMANN T, HILLER M, SCHRAMM D., An Active Suspension System for Simulation of Ship Maneuvers in Wind Tunnels, (2010)
  • [10] Test facilities