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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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Impact time control guidance with field-of-view constraint accounting for uncertain system lag
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PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING 2016年 第3期230卷 515-529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 with seeker's field-of-view constraint in the presence of uncertain system lag is addressed. A novel two-step control approach based impact time control guidance law wit... 详细信息
来源: 评论
Sliding mode control based impact angle control guidance considering the seeker's field-of-view constraint
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ISA TRANSACTIONS 2016年 61卷 49-59页
作者: Wang, Xingliang Zhang, Youan Wu, Huali Naval Aeronaut & Astronaut Univ Dept Control Engn ErMa Rd 188 Zhifu Dist 264001 Yantai Peoples R China
The problem of impact angle control guidance for a field-of-view constrained missile against non-maneuvering or maneuvering targets is solved by using the sliding mode control theory. The existing impact angle control... 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
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
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 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
Koopman Operator-Based Integrated Guidance and Control for Strap-Down High-Speed Missiles
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IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY 2024年 第6期32卷 2436-2443页
作者: Zhou, Min Lu, Mingfei Hu, Guanjie Guo, Zongyi Guo, Jianguo Northwestern Polytech Univ Inst Precis Guidance & Control Xian 710072 Peoples R China XianJiaotong Univ Inst Artificial Intelligence & Robot Xian 710049 Peoples R China
This work focuses on addressing the challenges of integrated guidance and control (IGC) for strap-down high-speed missiles with nonlinearities and field-of-view constraints. To achieve this, a data-driven prediction m... 详细信息
来源: 评论
Polynomial shaping based three-dimensional impact angle and field-of-view constrained guidance
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AEROSPACE SCIENCE AND TECHNOLOGY 2024年 147卷
作者: Surve, Prajakta Maity, Arnab Kumar, Shashi Ranjan Indian Inst Technol Dept Aerosp Engn Mumbai 400076 India
This paper proposes a polynomial-based three-dimensional (3D) impact angle-constrained guidance law considering the seeker's field-of-view (FOV) bound. The guidance laws are derived using nonlinear coupled dynamic... 详细信息
来源: 评论
Three-dimensional nonsingular impact angle guidance strategy with physical constraints
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ISA TRANSACTIONS 2022年 131卷 476-488页
作者: Yang, Xiao-yan Zhang, Yu-chen Song, Shen-min Harbin Inst Technol Sch Astronaut Harbin 150001 Heilongjiang Peoples R China
In this study, two nonsingular three-dimensional (3D) guidance strategies to intercept a stationary target with desired impact angles, subject to nonlinear coupled dynamics, field-of-view (FOV) limit and lateral accel... 详细信息
来源: 评论
Barrier Lyapunov Function Based Integrated Missile Guidance and Control Considering Phased Array Seeker Disturbance Rejection Rate
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IEEE ACCESS 2022年 10卷 31070-31083页
作者: Lin, Shih-Yao Wang, Jiang Wang, Wei Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China
A two-dimensional missile-target engagement geometry is established considering the effect of the disturbance rejection rate (DRR) problem caused by phased array radar beam pointing error and radome refraction error i... 详细信息
来源: 评论