Fuzzy linear/nonlinear active disturbance rejection switching control and its application

被引:0
作者
Wu Z. [1 ]
Deng C. [1 ]
Wen H. [2 ]
机构
[1] School of Electrical and New Energy, China Three Gorges University, Yichang
[2] 710 Institute of China Shipbuilding Industry Corporation, Yichang
来源
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 09期
基金
中国国家自然科学基金;
关键词
Active Disturbance Rejection Control (ADRC); Fuzzy rule; Jamming bomb; Roll angle; Switching control;
D O I
10.7527/S1000-6893.2020.24710
中图分类号
学科分类号
摘要
A fuzzy linear/nonlinear active disturbance rejection switching controller is proposed to deal with the strong nonlin-ear interference and the influence of model uncertainty encountered by the jamming bomb in the combat process. Firstly, mathematical models with the flywheel angular velocity as the controlled variable and the rolling angle as the controlled variable are established for the roll motion simulation device of the jamming projectile. The fuzzy rules are used to improve the linear/nonlinear active disturbance rejection switching control conditions, so as to achieve more stable fuzzy soft switching. Then, the strategies of the closed inner loop of Active Disturbance Rejection Control (ADRC) of flywheel angular velocity and the closed outer loop of fuzzy linear/nonlinear active disturb-ance rejection switching control of roll angle are used. Finally, the simulation model and experimental platform of the system are built. The simulation and experimental results show that the controller has the advantages of linear and nonlinear ADRC, and has high applicability. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
引用
收藏
相关论文
共 22 条
  • [1] ZHANG J, CHEN D, FANG S D., Research on operational use of active communication jamming shell in typical environment, Journal of Projectiles, Rockets, Missiles and Guidance, 40, 2, pp. 15-18, (2020)
  • [2] LIU S T, CHEN Q, GAO D H., Jamming effectiveness evaluation for shipborne surface-type infrared decoy defensing anti-ship missile, Laser & Infrared, 44, 9, pp. 1025-1029, (2014)
  • [3] NESLINE F W, WELLS B H, ZARCHAN P., Combined optimal/classical approach to robust missile autopilot design, Journal of Guidance, Control and Dynamics, 4, 3, pp. 316-322, (1981)
  • [4] RODDY D J, IRWIN G W, WILSON H., Approaches to roll-loop design for BTT CLOS Guidance, IEE Proceedings D Control Theory and Applications, 132, 6, (1985)
  • [5] PARKES N E, ROBERTS A P, WILSON H., Roll loop design for bank-to-turn guidance by polynomial methods, IEE Proceedings D Control Theory and Applications, 140, 6, (1993)
  • [6] LIU B, GAO S, HE N, Et al., Missile sub-channel simulation based on PID control, Electronic Design Engineering, 17, 11, pp. 97-99, (2009)
  • [7] TANG B T, DONG B, YU Y F., Autopilot design for BTT missile based on model reference variable structure control, Computer Measurement & Control, 19, 1, pp. 105-107, (2011)
  • [8] LI Z J, XIA Y Q, SU C Y, Et al., Missile guidance law based on robust model predictive control using neural-network optimization, IEEE Transactions on Neural Networks and Learning Systems, 26, 8, pp. 1803-1809, (2015)
  • [9] DONG Z, CHEN J B, SONG C L, Et al., Design of longitudinal control system for target missiles based on fuzzy adaptive PID control, 2017 29th Chinese Control and Decision Conference (CCDC), pp. 398-402, (2017)
  • [10] TRIVEDI P K, BANDYOPADHYAY B, MAHATA S, Et al., Roll stabilization: A higher-order sliding-mode approach, IEEE Transactions on Aerospace and Electronic Systems, 51, 3, pp. 2489-2496, (2015)