[1]周俊,江驹,余朝军,等.改进神经网络动态逆着舰控制方法[J].哈尔滨工程大学学报,2018,39(10):1649-1654.[doi:10.11990/jheu.201705004]
 ZHOU Jun,JIANG Ju,YU Chaojun,et al.Carrier aircraft dynamic inversion landing control based on improved neural network[J].hebgcdxxb,2018,39(10):1649-1654.[doi:10.11990/jheu.201705004]
点击复制

改进神经网络动态逆着舰控制方法(/HTML)
分享到:

《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
39
期数:
2018年10期
页码:
1649-1654
栏目:
出版日期:
2018-10-05

文章信息/Info

Title:
Carrier aircraft dynamic inversion landing control based on improved neural network
作者:
周俊 江驹 余朝军 肖东
南京航空航天大学 自动化学院, 江苏 南京 210016
Author(s):
ZHOU Jun JIANG Ju YU Chaojun XIAO Dong
College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
关键词:
舰载机着舰建模误差舰艉流神经网络自适应动态逆
分类号:
V249.122
DOI:
10.11990/jheu.201705004
文献标志码:
A
摘要:
针对舰载机着舰过程中存在建模误差和舰艉流干扰问题,本文提出一种基于改进神经网络的动态逆控制方法,用以提高着舰控制器的精度和速度。通过在动态逆控制中引入神经网络,对模型误差进行动态补偿,以满足控制器对精度的要求。对神经网络进行改进,引入自适应学习率,提高了网络的收敛速度。仿真结果表明:改进的神经网络动态逆方法对建模误差有较好的抑制作用,收敛速度大大提高,稳态误差趋于零;对舰艉气流有很好的抑制作用,有效维持舰载机着舰姿态和速度,保证舰载机安全着舰。

参考文献/References:

[1] 田瑾, 赵廷弟. 舰载机着舰安全的多维状态空间分析[J]. 北京航空航天大学学报, 2011, 37(2):155-160.TIAN Jin, ZHAO Tingdi. Multi-dimensional state space model to aircraft-deck landing safety[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(2):155-160.
[2] SHASTRY A K, PATTANAIK A, KOTHARI M. Neuro-adaptive augmented dynamic inversion controller for quadrotors[J]. Ifac papersonline, 2016, 49(1):302-307.
[3] PIAZZI A, VISIOLI A. Robust set-point constrained regulation via dynamic inversion[J]. International journal of robust & nonlinear control, 2015, 11(1):1-22.
[4] CAMPBELL S F, KANESHIGE J T. A nonlinear dynamic inversion L 1, adaptive controller for a Generic Transport Model[C]//American Control Conference. IEEE, 2010:862-867.
[5] 朱家强, 郭锁凤. 一种在线神经网络在补偿飞机模型不确定性误差中的应用[J]. 南京航空航天大学学报, 2003, 35(1):86-90.ZHU Jiaqiang, GUO Suofeng. Application of online neural network for compensating uncertain error of aircraft model[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2003, 35(1):86-90.
[6] 朱家强, 朱纪洪, 郭锁凤, 等. 基于神经网络的鲁棒自适应逆飞行控制[J]. 控制理论与应用, 2005, 22(2):182-188.ZHU Jiaqiang, ZHU Jihong, GUO Suofeng, et al. Neural network based robust dynamic inversion flight control[J]. Control theory & applications, 2005, 22(2):182-188.
[7] 朱齐丹, 孟雪, 张智. 基于非线性动态逆滑模的纵向着舰系统设计[J]. 系统工程与电子技术, 2014, 36(4):2037-2042.ZHU Qidan, MENG Xue, ZHANG Zhi. Design of longitudinal carrier landing system using nonlinear dynamic inversion and sliding mode control[J]. Systems engineering and electronics, 2014, 36(4):2037-2042.
[8] 韩英华, 范彦铭. 基于非线性动态逆的无人机自动着陆控制系统[J]. 航空学报, 2008, 29(9):S66-S72.HAN Yinghua, FAN Yanming. Control system of automatic landing of UAV based on nonlinear dynamic inversion[J]. Acta aeronautica et astronautica sinica, 2008, 29(9):S66-S72.
[9] CRASSIDIS J, MOOK D. Robust control design of an automatic carrier landing system[C]//Robust Control Design of an Automatic Carrier Landing System. New York, 2013.
[10] 鲁可, 袁锁中. 层叠结构动态逆在无人战斗机控制中的应用[J]. 飞行力学, 2012. 30(5):463-465, 469.LU Ke, YUAN Suozhong. Hierarchy-structured dynamic inversion in the UCAV control[J]. Flight dynamics, 2012, 30(5):463-465, 469.
[11] LUNGU M, LUNGU R, TUTUNEA D. Control of aircraft landing using the dynamic inversion and the H-inf control[C]//Carpathian Control Conference. IEEE, 2016:461-466.
[12] ABASPOUR A, SADEGHI M, SADATI S H. Using fuzzy logic in dynamic inversion flight controller with considering uncertainties[C]//Fuzzy Systems. IEEE, 2013:1-6.
[13] 朱家强, 郭锁凤. 基于神经网络的超机动飞机自适应重构控制[J]. 航空学报, 2003, 24(3):246-250.ZHU Jiaqiang, GUO Suofeng. Neural-net based adaptive reconfigurable control for a super-maneuverable aircraft[J]. Acta aeronautica et astronautica sinica, 2003, 24(3):246-250.
[14] 史青海. 舰载机着舰控制技术研究[D]. 哈尔滨:哈尔滨工程大学, 2006.SHI Qinghai. Study on control technology for carrier aircraft landing[D]. Harbin:Harbin Engineering University, 2006.
[15] Department of defense handbook flying qualities of pilot aircraft[EB/OL].[2008-02-20].
[16] 朱荣刚, 姜长生, 邹庆元, 等. 新一代歼击机超机动飞行的动态逆控制[J]. 航空学报, 2003, 24(3):242-245.ZHU Ronggang, JIANG Changesheng, ZOU Qingyuan, et al. Study on dynamic inversion control and simulation of supermaneuverable flight of the new generation fighter[J]. Acta aeronautica et astronautica sinica, 2003, 24(3):242-245.
[17] 李怡勇, 沈怀荣. 无人机神经网络动态逆控制器设计研究[J]. 航天控制, 2009, 27(5):3-6.LI Yiyong, SHEN Huairong. Dynamic inversion controller design of UAV based on NN[J]. Aerospace control, 2009, 27(5):3-6.

相似文献/References:

[1]孙晓羽,王振清,吕红庆,等.飞机着舰拦阻动力学分析[J].哈尔滨工程大学学报,2010,(01):69.
 SUN Xiao yu,WANG Zhen qing,L Hong qing,et al.Dynamic analysis of carrier aircraft landing[J].hebgcdxxb,2010,(10):69.
[2]朱齐丹,李新飞,喻勇涛.考虑载荷突卸的舰载机弹射起飞动力学分析[J].哈尔滨工程大学学报,2012,(09):1150.[doi:10.3969/j.issn.1006-7043. 201111078]
 ZHU Qidan,LI Xinfei,YU Yongtao.Analysis of dynamic characteristics of catapult launch for a carrier-based aircraft with sudden load discharge[J].hebgcdxxb,2012,(10):1150.[doi:10.3969/j.issn.1006-7043. 201111078]
[3]刘钦辉,邱长华,王能建.考虑空间约束的舰载机作业调度模型研究[J].哈尔滨工程大学学报,2012,(11):1435.[doi:10.3969/j.issn.1006-7043. 201109024]
 LIU Qinhui,QIU Changhua,WANG Nengjian.Study on ship-based aircraft operation scheduling model considering spatial restriction[J].hebgcdxxb,2012,(10):1435.[doi:10.3969/j.issn.1006-7043. 201109024]
[4]朱齐丹,闻子侠,张智,等.舰载机着舰侧回路混合H∞/H2模型参考LPV控制[J].哈尔滨工程大学学报,2013,(01):83.[doi:10.3969/j.issn.1006-7043.201204043]
 ZHU Qidan,WEN Zixia,ZHANG Zhi,et al.Carrier aircraft landing mixed H∞/H2 LPV model reference control during powered approach[J].hebgcdxxb,2013,(10):83.[doi:10.3969/j.issn.1006-7043.201204043]
[5]夏国清,陈红召.面向使用可用度的舰载机可修备件库存模型[J].哈尔滨工程大学学报,2013,(01):98.[doi:10.3969/j.issn.1006-7043. 201203070]
 XIA Guoqing,CHEN Hongzhao.Operational availability oriented inventory model for repairable spare parts of embarked air-wings[J].hebgcdxxb,2013,(10):98.[doi:10.3969/j.issn.1006-7043. 201203070]
[6]张智,林圣琳,夏桂华,等.舰载机甲板调运过程避碰路径规划研究[J].哈尔滨工程大学学报,2014,(01):9.[doi:10.3969/j.issn.1006-7043.201304025]
 ZHANG Zhi,LIN Shenglin,XIA Guihua,et al.Collision avoidance path planning for an aircraft in scheduling process on deck[J].hebgcdxxb,2014,(10):9.[doi:10.3969/j.issn.1006-7043.201304025]
[7]夏桂华,董然,孟雪,等.舰载机着舰的动力学建模[J].哈尔滨工程大学学报,2014,(04):445.[doi:10.3969/j.issn.10067043.201309033]
 XIA Guihua,DONG Ran,MENG Xue,et al.Research on the dynamic modeling for the landing of a carrierbased aircraft[J].hebgcdxxb,2014,(10):445.[doi:10.3969/j.issn.10067043.201309033]
[8]张智,闻子侠,朱齐丹,等.舰载机阻拦过程动力学仿真[J].哈尔滨工程大学学报,2014,(05):571.[doi:10.3969/j.issn.10067043.201305035]
 ZHANG Zhi,WEN Zixia,ZHU Qidan,et al.Kinetic simulation of shipboard arresting system[J].hebgcdxxb,2014,(10):571.[doi:10.3969/j.issn.10067043.201305035]
[9]李新飞,王立辉,朱齐丹,等.考虑弹射起飞的航母剩余甲板长度研究[J].哈尔滨工程大学学报,2015,(01):113.[doi:10.3969/j.issn.1006-7043.201310039]
 LI Xinfei,WANG Lihui,ZHU Qidan,et al.Analysis of deck edge distance taking into account the catapult launch[J].hebgcdxxb,2015,(10):113.[doi:10.3969/j.issn.1006-7043.201310039]
[10]张智,李佳桐,董然,等.针对舰艉流抑制的ACLS纵向控制律优化设计[J].哈尔滨工程大学学报,2016,37(06):802.[doi:10.11990/jheu.201504065]
 ZHANG Zhi,LI Jiatong,DONG Ran,et al.Optimal design of longitudinal automatic carrier landing system for carrier air wake rejection[J].hebgcdxxb,2016,37(10):802.[doi:10.11990/jheu.201504065]
[11]王立辉,朱齐丹,李新飞.液压式阻拦系统的数学建模及仿真[J].哈尔滨工程大学学报,2012,(03):330.[doi:10.3969/j.issn.1006-7043.201102018]
 WANG Lihui,ZHU Qidan,LI Xinfei.The mathematical model and simulation of a hydraulic arresting gear system[J].hebgcdxxb,2012,(10):330.[doi:10.3969/j.issn.1006-7043.201102018]

备注/Memo

备注/Memo:
收稿日期:2017-05-02。
基金项目:国家自然科学基金项目(61673209);南京航空航天大学研究生创新基地(实验室)开放基金项目(kfjj20160318).
作者简介:周俊(1992-),男,硕士研究生;江驹(1963-),男,教授,博士生导师.
通讯作者:周俊,E-mail:zj031110319@nuaa.edu.cn.
更新日期/Last Update: 2018-10-10