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基于在线学习的机载光电系统扩张状态观测器参数整定研究 被引量:3

Parameter Setting of Extended State Observer in Airborne Electro-Optical System Based on Online Learning
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摘要 针对非线性动态系统的扩张状态观测器(ESO)参数整定问题,建立了基于BP神经网络的参数整定模型。采用在线梯度下降法进行网络训练以保证对动态系统的学习能力,并引入了IDBD算法,利用输入数据的信息和学习过程中的经验实现学习速率的自适应调整,以改进在线梯度下降法的适应性。数字仿真表明,该参数整定模型较传统的参数整定模型具有动态性能好、精度高等优点,能够提高非线性系统扩张状态观测器参数的动态整定精度,进而在一定程度上改善自抗扰控制器的系统控制性能。 In order to solve the problem of parameter setting of the extended state observer used in nonlinear dynamic system,a parameter setting model based on BP neural network is established.The online gradient descent method is used to train the network so as to ensure the learning ability of the dynamic system.The incremental Delta-Bar-Delta algorithm is introduced,and the information of input data and learning experience are used to realize the adaptive adjustment of the learning rate and improve the adaptability of the online gradient descent method.It can be seen from the numerical simulation that the parameter setting model possesses the advantages of good dynamic performance and high accuracy compared with the traditional parameter setting model,and it can improve the dynamic setting accuracy of the parameters of the extended state observer of the nonlinear system,so that the controlling performance of the ADRC system is improved to a certain extent.
作者 周德召 刘晓东 李佳庆 王合龙 ZHOU De-zhao;LIU Xiao-dong;LI Jia-qing;WANG He-long(Luoyang Institute of Electro-Optical Equipment AVIC Luoyang 471000,China;PLA Air Force Equipment Department Beijing 100843,China;Beijing Institute of Technology Beijing 100081,China;Science and Technology on Electro-Optical Control Laboratory,Luoyang 471000,China)
出处 《电光与控制》 CSCD 北大核心 2019年第8期43-47,共5页 Electronics Optics & Control
关键词 机载光电系统 前向神经网络 在线学习 自抗扰控制 扩张状态观测器 airborne electro-optical system forward neural network online learning active disturbance rejection controller extended state observer
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  • 1韩京清.自抗扰控制技术[J].前沿科学,2007,1(1):24-31. 被引量:455
  • 2宋英麟,鲜斌,茹滨超,曹美会.无人机微型姿态航向系统数据处理[J].中南大学学报(自然科学版),2013,44(S2):89-93. 被引量:15
  • 3李海生,朱学峰.自抗扰控制器参数整定与优化方法研究[J].控制工程,2004,11(5):419-423. 被引量:50
  • 4韩京清,王伟.非线性跟踪─微分器[J].系统科学与数学,1994,14(2):177-183. 被引量:405
  • 5Costa R R,Chu Q P,Mulder J A.Reentry flight controller design using nonlinear dynamic inversion[J].Journal of Spacecraft and Rockets,2003,40(1):64-71.
  • 6Shtessel Y,McDuffie J.Sliding mode control of the X-33 vehicle in launch and re-entry modes[C]// Proc.of AIAA Guidance,Navigation and Control Conference,AIAA Press,USA,1998:1352-1362.
  • 7Oort E R,Sonneveldt L,Sonneveldt C Q P,et al.A Comparison of adaptive nonlinear control designs for an over-actuated fighter aircraft model[C]// Proc.of AIAA Guidance,Navigation and Control Conference and Exhibit,Honolulu,AIAA press,2008:1-20.
  • 8Mracek C P,Cloutier J R.Full envelope missile longitudinal autopilot design using the state-dependent riccati equation method[M]// Sivasundaram S.Nonlinear problems in aviation and aerospace.Gordon and Breach Science Publishers,2000:57-76.
  • 9Xin M,Balakrishnan S N.Missile autopilot design using a new suboptimal nonlinear control method[C]// IEE Proc.of 41st Aerospace Sciences Meeting and Exhibit,Reno,2003:577-584.
  • 10Suresh S,Omkar S N,Mani V,et al.Direct adaptive neural flight controller for F-8 fighter aircraft[J].Journal of Guidance,Control,and Dynamics,2006,29(2):454-464.

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