Three-dimensional cooperative guidance law for multiple missiles with impact angle constraint
Author:
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/5971804/9316325/09316409.pdf?arnumber=9316409
Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Time-to-go based three-dimensional multi-missile spatio-temporal cooperative guidance law: A novel approach for maneuvering target interception;ISA Transactions;2024-06
2. Finite-time Cooperative Guidance Laws of Impact Time and Angle with Input Saturation Constraint;Proceedings of the 2024 3rd International Symposium on Intelligent Unmanned Systems and Artificial Intelligence;2024-05-17
3. Review of space target positioning algorithms based on space-based optical detection;CHIN SPACE SCI TECHN;2024
4. A Formation Control Method for Leader-Follower Aircraft Based on Particle Swarm Optimization;Lecture Notes in Electrical Engineering;2024
5. Distributed adaptive cooperative guidance against maneuvering targets with time-varying terminal angle constraint and overload saturation;Journal of the Franklin Institute;2023-11
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