[1]甄子洋,陶钢,江驹,等.无人机自动撞网着舰轨迹自适应跟踪控制[J].哈尔滨工程大学学报,2017,38(12):1922-1927.[doi:10.11990/jheu.201612061]
 ZHEN Ziyang,TAO Gang,JIANG Ju,et al.Adaptive tracking control of automatic net landing trajectory for carrier-based unmanned aerial vehicle[J].hebgcdxxb,2017,38(12):1922-1927.[doi:10.11990/jheu.201612061]
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
38
期数:
2017年12期
页码:
1922-1927
栏目:
出版日期:
2017-12-25

文章信息/Info

Title:
Adaptive tracking control of automatic net landing trajectory for carrier-based unmanned aerial vehicle
作者:
甄子洋1 陶钢12 江驹1 王新华1
1. 南京航空航天大学 自动化学院, 南京 210016;
2. 弗吉尼亚大学 电气与计算机工程学院, 美国 夏洛茨维尔 22904-4743
Author(s):
ZHEN Ziyang1 TAO Gang12 JIANG Ju1 WANG Xinhua1
1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
2. Department of Electrical and Computer Engineering, University of Virginia, Charlottesville 22904-4743, USA
关键词:
无人机自动着舰撞网着舰轨迹自适应控制飞行控制轨迹跟踪气动数据六自由度非线性数学模型
分类号:
TP273
DOI:
10.11990/jheu.201612061
文献标志码:
A
摘要:
针对舰载小型固定翼无人机的自动撞网着舰技术进行研究,基于无人机气动数据建立六自由度非线性数学模型。构建无人机撞网着舰引导与控制系统结构,设计了撞网着舰三维基准下滑轨迹,采用滤波引导方法设计纵向和侧向引导律。在无人机模型参数未知的情况下,采用模型参考自适应控制分别设计了升降舵、油门、副翼和方向舵控制通道的自适应控制律。舰载无人机非线性模型的数值仿真结果表明,自适应飞行控制方法下的无人机具有较精确的着舰轨迹跟踪性能。

参考文献/References:

[1] Anon. Naval interest in shipborne unmanned air vehicles[J]. Naval architect, 1997:45-46.
[2] PERRY J D. Navy unmanned air systems 1915-2011[C]//Proceedings of AIAA Centennial of Naval Aviation Forum "100 Years of Achievement and Progress".[S.l.], 2011.
[3] 杨一栋. 舰载飞机着舰引导与控制[M]. 北京:国防工业出版社, 2006.YANG Yidong. Carrier landing guidance and control of carrier-based aircraft[M]. Beijing:National Defense Industry Press, 2006.
[4] 甄子洋, 王新华, 江驹, 等. 舰载机自动着舰引导与控制[J]. 航空学报, 2017, 38(2):1-22.ZHEN Ziyang, WANG Xinhua, JIANG Ju, et al. Research progress in guidance and control of automatic carrier landing of carrier-based aircraft[J]. Acta aeronautica ET astronautica sinica, 2017, 38(2):1-22.
[5] 杨一栋, 甄子洋, 徐佳龙, 等. 无人机着舰制导与控制[M]. 北京:国防工业出版社, 2013.YANG Yidong, ZHEN Ziyang, XU Jialong, et al. UAV carrier landing guidance and control[M]. Beijing:National Defense Industry Press, 2013.
[6] 李若兰, 甄子洋, 龚华军. 基于趋近律滑模最优控制的无人机撞网回收轨迹控制[J]. 电光与控制, 2014, 21(9):58-60, 84.LI Ruolan, ZHEN Ziyang, GONG Huajun. Trajectory control of a UAV during net recovery based on sliding mode control and optimal control[J]. Electronics optics and control, 2014, 21(9):58-60, 84.
[7] ZHENG F Y, GONG H J, ZHEN Z Y. Adaptive constraint backstepping fault tolerant control for small carrier UAV with uncertain parameters[J]. Proceedings of the institution of mechanical engineers, Part G:journal of aerospace engineering, 2016, 230:407-425.
[8] ZHENG F Y, ZHEN Z Y, GONG H J. Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults[J]. Journal of systems engineering and electronics, 2017, 28(2):322-337.
[9] TAO G. Adaptive control design and analysis[M].[S.l.]:Wiley-Interscience, 2003.
[10] GOODWIN G C, GRAEBE S F, SALGADO M E. Control system design[M]. Upper Saddle River:Prentice-Hall, 2001.

相似文献/References:

[1]朱齐丹,王立鹏,张智,等.舰载机着舰纵向时变风险权值矩阵预测控制[J].哈尔滨工程大学学报,2016,37(11):1532.[doi:10.11990/jheu.201509033]
 ZHU Qidan,WANG Lipeng,ZHANG Zhi,et al.Model predictive control of the longitudinal time-varying risk weight matrix for a carrier-based aircraft landing[J].hebgcdxxb,2016,37(12):1532.[doi:10.11990/jheu.201509033]

备注/Memo

备注/Memo:
收稿日期:2016-12-17。
基金项目:国家自然科学基金项目(61304223,61673209,61533008);航空科学基金项目(2016ZA52009);中央高校基本科研业务费专项资金项目(NS2017015).
作者简介:甄子洋(1981-),男,副教授,硕士生导师;陶钢(1958-),男,教授,博士生导师,"千人计划"特聘教授;江驹(1962-),男,教授,博士生导师.
通讯作者:甄子洋,E-mail:zhenziyang@nuaa.edu.cn.
更新日期/Last Update: 2018-01-13