Optimal Look-Angle Guidance with Field-of-View and Impact Angle Constraints for Strapdown Munition

被引:2
作者
Wang, Peng [1 ]
Fan, Jun-fang [2 ]
Chen, Shi-wei [1 ,2 ]
Wang, Hai-sen [2 ]
Wang, Wei [1 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Beijing Informat Sci & Technol Univ, Beijing Key Lab High Dynam Nav Technol, Beijing 100192, Peoples R China
基金
中国国家自然科学基金;
关键词
LAW;
D O I
10.1155/2022/6057998
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A strapdown seeker with limited field-of-view (FOV) can simplify and decrease cost of the guidance system for a munition. However, the inherent defect of the strapdown seeker is that it could not provide the necessary line-of-sight (LOS) angular information for typical guidance application. This paper proposed an optimal look-angle guidance law (OLAGL) which directly utilized seeker angle information and satisfies the constraints of FOV and terminal impact angle. The coefficient determination, effects of switching threshold, and gains for the guidance law are analyzed and detailed. The simulation results compared with typical trajectory shaping guidance for a ground target show that the presented guidance law can satisfy the impact angle constraint under the limitation of FOV and provide a well engineering reference.
引用
收藏
页数:13
相关论文
共 22 条
[1]  
Fan J.F., 2016, 2016 16 INT C CONTRO, DOI [10.1109/ICCAS.2016.7832432, DOI 10.1109/ICCAS.2016.7832432]
[2]   Field-of-view limited guidance with impact angle constraint and feasibility analysis [J].
Hu, Qinglei ;
Cao, Ruihao ;
Han, Tuo ;
Xin, Ming .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 114
[3]   The Tianwen-1 Guidance, Navigation, and Control for Mars Entry, Descent, and Landing [J].
Huang, Xiangyu ;
Li, Maodeng ;
Wang, Xiaolei ;
Hu, Jinchang ;
Zhao, Yu ;
Guo, Minwen ;
Xu, Chao ;
Liu, Wangwang ;
Wang, Yunpeng ;
Hao, Ce ;
Xu, Lijia .
SPACE-SCIENCE & TECHNOLOGY, 2021, 2021
[4]   Off-Target Look Angle Control Guidance Law for Moving Targets [J].
Jeon, In-Soo ;
Karpenko, Mark .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2019, 42 (11) :2432-2442
[5]  
Kim D, 2011, 2011 11TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS), P969
[6]   Look-Angle-Shaping Guidance Law for Impact Angle and Time Control With Field-of-View Constraint [J].
Kim, Hyeong-Geun ;
Lee, Jun-Yong ;
Kim, Hyoun Jin ;
Kwon, Hyuck-Hoon ;
Park, Jang-Seong .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2020, 56 (02) :1602-1612
[7]  
Kim HG, 2016, IEEE DECIS CONTR P, P4160, DOI 10.1109/CDC.2016.7798900
[8]   TERMINAL GUIDANCE FOR IMPACT ATTITUDE ANGLE CONSTRAINED FLIGHT TRAJECTORIES [J].
KIM, M ;
GRIDER, KV .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1973, AES9 (06) :852-859
[9]   A Hybrid Guidance Law for a Strapdown Seeker to Maintain Lock-on Conditions against High Speed Targets [J].
Lee, Chae Heun ;
Hyun, Chul ;
Lee, Jang Gyu ;
Choi, Jin Yung ;
Sung, Sangkyung .
JOURNAL OF ELECTRICAL ENGINEERING & TECHNOLOGY, 2013, 8 (01) :190-196
[10]   Practical generalized optimal guidance law with impact angle constraint [J].
Lee, Chang-Hun ;
Ryu, Moo-Yong .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (10) :3790-3809