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finite-time convergent terminal guidance law design based on stochastic fast smooth second-order sliding mode 谢谢 发自小木虫Android客户端 |
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hopfliking: 回帖置顶 2017-10-09 19:59:13
hopfliking: 金币+10 2017-10-09 20:03:52
心静_依然: LS-EPI+1, 感谢应助 2017-10-11 12:25:57
心静_依然: LS-EPI+1, 感谢应助 2017-10-11 12:26:20
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hopfliking: 回帖置顶 2017-10-09 19:59:13
hopfliking: 金币+10 2017-10-09 20:03:52
心静_依然: LS-EPI+1, 感谢应助 2017-10-11 12:25:57
心静_依然: LS-EPI+1, 感谢应助 2017-10-11 12:26:20
心静_依然: 应助指数+1, 感谢应助 2017-10-11 12:26:37
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关闭 Web of Science 第 1 页 (记录 1 -- 1) 上一页 (不活动) [ 1 ] 下一页 (不活动) 打印此页 第 1 条，共 1 条 标题: Finite-time convergent terminal guidance law design based on stochastic fast smooth second-order sliding mode 作者: Yang, PF (Yang, Peng-fei); Fang, YW (Fang, Yang-wang); Wu, YL (Wu, You-li); Yong, XJ (Yong, Xiao-ju) 来源出版物: OPTIK 卷: 127 期: 15 页: 6036-6049 DOI: 10.1016/j.ijleo.2016.04.037 出版年: 2016 Web of Science 核心合集中的 "被引频次": 1 被引频次合计: 1 使用次数 (最近 180 天): 1 使用次数 (2013 年至今): 6 引用的参考文献数: 24 摘要: A novel finite-time convergent terminal guidance law, based on stochastic fast smooth second-order sliding mode control theory, is proposed in order to handle the track imprecision caused mainly by inertial lag, model uncertainties and atmospheric environment disturbances, as well as the stochastic noise caused by target maneuver term. The missile interceptor guidance system against targets performing evasive maneuvers is considered. The target maneuver model is employed to alleviate the dependence of the perfect knowledge of the range to target and the range rate as well as the limitation to target normal acceleration. Considering that the system is driven by additive noise, which do not have any equilibrium, a new concept of finite-time mean-square practical convergence is presented. And based on this concept, the finite-time convergence property of proposed guidance law is deduced. The availability and effectiveness of the proposed guidance law is illustrated through computer simulations. The results show that the proposed guidance law can realize finite-time convergence, and it has strong robustness against bounded uncertainties as well as the stochastic noise. The proposed guidance law does not has violent high-frequency chattering, which guarantees the tracking accuracy. (C) 2016 Elsevier GmbH. All rights reserved. 入藏号: WOS:000377323400035 语种: English 文献类型: Article 作者关键词: Stochastic fast smooth second-order sliding mode; Finite-time convergence; Mean-square practical convergence; Terminal missile guidance law KeyWords Plus: MISSILE; SYSTEMS 地址: [Yang, Peng-fei; Fang, Yang-wang; Wu, You-li] Air Force Engn Univ, Sch Aeronaut & Astronaut Engn, Xian 710038, Peoples R China. [Yong, Xiao-ju] Air Force First Aviat Coll, Xinyang 464000, Peoples R China. 通讯作者地址: Yang, PF (通讯作者),Air Force Engn Univ, Sch Aeronaut & Astronaut Engn, Xian 710038, Peoples R China. 电子邮件地址: pfyang1988@126.com 出版商: ELSEVIER GMBH, URBAN & FISCHER VERLAG 出版商地址: OFFICE JENA, P O BOX 100537, 07705 JENA, GERMANY Web of Science 类别: Optics 研究方向: Optics IDS 号: DN8IW ISSN: 0030-4026 29 字符的来源出版物名称缩写: OPTIK ISO 来源出版物缩写: Optik 来源出版物页码计数: 14 基金资助致谢: 基金资助机构 授权号 National Natural Science Foundation of China 60874040 Natural Science Foundation of Shaanxi Province 2014JQ8339 The authors would like to express their thanks for the support from the National Natural Science Foundation of China (No. 60874040) and the Natural Science Foundation of Shaanxi Province (No. 2014JQ8339). 公开访问: No 输出日期: 2017-10-09 关闭 Web of Science 第 1 页 (记录 1 -- 1) 上一页 (不活动) [ 1 ] = 打印此页 © 2017 CLARIVATE ANALYTICS 使用条款 隐私策略 反馈 |
2楼2017-10-09 16:43:59
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hopfliking: 金币+10 2017-10-10 23:02:12
hopfliking: 金币+10 2017-10-10 23:02:12
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