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检索条件"主题词=Field-of-view constraint"
38 条 记 录,以下是11-20 订阅
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Asymmetric integral barrier Lyapunov function-based three-dimensional integrated guidance and control design with field-of-view constraint and input saturation
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ADVANCES IN MECHANICAL ENGINEERING 2024年 第3期16卷
作者: Feng, Dan Hou, Mingshan Wang, Wencong Wang, Dongyue Northwestern Polytech Univ Sch Automat 1 Dongxiang Rd Xian 710072 Shaanxi Peoples R China
This paper proposes an adaptive integrated guidance control (IGC) scheme for the flight vehicle intercepting the maneuvering target with asymmetric field-of-view angle constraint, input magnitude and rate saturation, ... 详细信息
来源: 评论
Impact time control guidance law with field of view constraint
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AEROSPACE SCIENCE AND TECHNOLOGY 2014年 39卷 361-369页
作者: Zhang, Youan Wang, Xingliang Wu, Huali Naval Aeronaut & Astronaut Univ Dept Control Engn Yantai 264001 Peoples R China
The problem of Impact Time Control Guidance (ITCG) with field-of-view (FOV) constraint is investigated. The proposed ITCG law is a combination of the well-known Proportional Navigation Guidance (PNG) law and an additi... 详细信息
来源: 评论
Distributed cooperative guidance law without numerical singularity with field-of-view angle constraint
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AERONAUTICAL JOURNAL 2024年 第1336期129卷 1515-1533页
作者: Liu, Z. Li, S. Ren, L. Ma, D. High Tech Inst Xian Xian Peoples R China Tsinghua Univ Dept Automat Beijing Peoples R China
A distributed cooperative guidance law without numerical singularities is proposed for the simultaneous attack a stationary target by multiple vehicles with field-of-view constraints. Firstly, the vehicle engagement m... 详细信息
来源: 评论
Integrated cooperative guidance and control of strapdown missiles
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PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING 2025年 第6期239卷 528-556页
作者: Huang, Xiaoyang Zhao, Bin Zhou, Jun Xie, Jingjie Zhao, Wanli Northwestern Polytech Univ Inst Precis Guidance & Control 127 West Youyi Rd Xian 710072 Peoples R China Univ Warwick Sch Engn Coventry England Sci & Technol Electroopt Informat Secur Control La Tianjin Peoples R China
This paper develops an innovative integrated cooperative guidance and control (ICGC) law for multiple strapdown missiles, and explicitly considers both the attitude dynamics and field-of-view (FOV) limitations of the ... 详细信息
来源: 评论
field-of-view limited guidance with impact angle constraint and feasibility analysis
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AEROSPACE SCIENCE AND TECHNOLOGY 2021年 114卷 106753-106753页
作者: Hu, Qinglei Cao, Ruihao Han, Tuo Xin, Ming Beihang Univ Sch Automat Sci & Elect Engn Beijing 100191 Peoples R China Aviat Ind Corp China Xian Flight Automat Control Res Inst Xian 710065 Peoples R China Univ Missouri Dept Mech & Aerosp Engn Columbia MO 65211 USA
A look angle shaping guidance law with impact angle and seeker's field-of-view (FOV) constraints considering the time-varying speed is proposed. A look angle profile with respect to the relative range is first con... 详细信息
来源: 评论
Integrated Guidance and Control Scheme for Unmanned Aerial Vehicle with Unknown Control Coefficient Accommodating Approach Angle and field-of-view constraints
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JOURNAL OF AEROSPACE ENGINEERING 2024年 第3期37卷 04024008-04024008页
作者: Ding, Yixin Guo, Zongyi Cao, Shiyuan Guo, Jianguo Oliveira, Tiago Roux Northwestern Polytech Univ Inst Precis Guidance & Control Xian 710072 Peoples R China State Univ Rio De Janeiro UERJ Dept Elect & Telecommun Engn DETEL BR-20550900 Rio De Janeiro RJ Brazil
This paper investigates the issue of integrated guidance and control (IGC) design for an unmanned aerial vehicle with an unknown control coefficient, approach angle constraint, and field-of-view limitations. Different... 详细信息
来源: 评论
Integrated cooperative guidance framework and cooperative guidance law for multi-missile
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Chinese Journal of Aeronautics 2018年 第3期31卷 546-555页
作者: Jianbo ZHAO Shuxing YANG School of Aerospace Engineering Beijing Institute of Technology Key Laboratory of Dynamics and Control of Flight Vehicle Ministry of Education
An integrated cooperative guidance framework for multi-missile cooperatively attacking a single stationary target is proposed in this paper by combining both the centralized and decentralized communication topologies.... 详细信息
来源: 评论
Two-phase guidance law for impact time control under physical constraints
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Chinese Journal of Aeronautics 2020年 第11期33卷 2946-2958页
作者: Yang TANG Xiaoping ZHU Zhou ZHOU Fei YAN National Key Laboratory of Science and Technology on UAV Northwestern Polytechnical UniversityXi’an 710065China UAV Research Institute Northwestern Polytechnical UniversityXi'an 710065China School of Aeronautics Northwestern Polytechnical UniversityXi'an 710072China
An impact-time-control guidance law is required for the simultaneous attack of suicide attack unmanned aerial *** on the nonlinear model,a two-phase guidance strategy is *** impact time is derived in a simple analytic... 详细信息
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A distributed cooperative guidance law for salvo attack of multiple anti-ship missiles
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Chinese Journal of Aeronautics 2015年 第5期28卷 1438-1450页
作者: Zhang Youan Wang Xingliang Wu Huali Department of Control Engineering Naval Aeronautical and Astronautical University
The consensus problem of impact time is addressed for multiple anti-ship missiles. A new distributed cooperative guidance law with the form of biased proportional navigation guidance (BPNG) is presented. The propose... 详细信息
来源: 评论
field-of-view and Impact Angle Constrained Guidance Law for Missiles With Time-Varying Velocities
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IEEE ACCESS 2019年 7卷 61717-61727页
作者: Liu, Bojun Hou, Mingshan Li, Yajun Northwestern Polytech Univ Sch Automat Xian 710072 Shaanxi Peoples R China
A novel nonlinear non-switching guidance strategy is proposed for missiles with time-varying velocities intercepting stationary targets, considering impact angle, seeker's field-of-view, and input saturation const... 详细信息
来源: 评论