[1]顾臣风,江驹,吴雨珊.近空间飞行器爬升段跟踪控制[J].哈尔滨工程大学学报,2016,37(11):1526-1531.[doi:10.11990/jheu.201503056]
 GU Chenfeng,JIANG Ju,WU Yushan.Tracking control for a near-space vehicle in the ascent phase[J].hebgcdxxb,2016,37(11):1526-1531.[doi:10.11990/jheu.201503056]
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近空间飞行器爬升段跟踪控制(/HTML)
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
37
期数:
2016年11期
页码:
1526-1531
栏目:
出版日期:
2016-11-25

文章信息/Info

Title:
Tracking control for a near-space vehicle in the ascent phase
作者:
顾臣风 江驹 吴雨珊
南京航空航天大学 自动化学院, 江苏 南京 210016
Author(s):
GU Chenfeng JIANG Ju WU Yushan
College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
关键词:
近空间飞行器跟踪控制爬升模态双幂次趋近律滑模控制参数不确定李雅普诺夫稳定性理论
分类号:
V249
DOI:
10.11990/jheu.201503056
文献标志码:
A
摘要:
在近空间飞行器加速爬升模态下,传统的滑模控制方法在处理不确定性问题时,存在收敛速度慢、鲁棒性不强和抖振严重等不足。针对这些问题,本文提出双幂次趋近律滑模控制方法来设计飞行控制器,从而实现飞行器爬升段轨迹的精确跟踪。将飞行器非线性模型进行精确反馈线性化处理,并利用李雅普诺夫稳定性理论进行稳定性分析。仿真分析了双幂次趋近律滑模控制方法和传统滑模控制方法的控制效果。结果表明:在处理具有参数不确定性和外界干扰的非线性系统时,双幂次趋近律滑模控制方法能够精确地跟踪指令信号,并且具有较强的稳定性和鲁棒性。

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备注/Memo

备注/Memo:
收稿日期:2015-03-18。
基金项目:国家自然科学基金项目(61304223);教育部高等学校博士学科点专项科研基金项目(20123218120015);南京航空航天大学研究生创新基地(实验室)开发基金项目(kfjj201420).
作者简介:顾臣风(1990-),男,硕士研究生;江驹(1963-),男,教授,博士生导师,博士.
通讯作者:顾臣风,E-mail:gcfunny@163.com.
更新日期/Last Update: 2016-12-03