In order to solve the interception problem for maneuvering target, a dynamic programming guidance law is proposed. Firstly, under the condition that the acceleration information of the target is unknown, according to the current position and velocity of the target, the optimization indexes including minimum remaining attack time and minimum miss distance are designed. Secondly, based on the above optimization indexes, considering the control constraints of interceptor missile, the online planning scheme of guidance command is proposed for non-game maneuvering target and game maneuvering target respectively. Finally, the simulation is designed to test the performance of the guidance law for targets with various maneuvering behaviors. The simulation results show that the dynamic programming guidance law can effectively guide the interceptor missile under control constraints to intercept maneuvering targets, and has good adaptability and convergence.
Dynamic Programming Guidance Law for Maneuvering Target
Lect. Notes Electrical Eng.
International Conference on Autonomous Unmanned Systems ; 2021 ; Changsha, China September 24, 2021 - September 26, 2021
Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021) ; Chapter : 238 ; 2413-2426
2022-03-18
14 pages
Article/Chapter (Book)
Electronic Resource
English
Fuzzy guidance law for intercepting maneuvering target
British Library Online Contents | 1998
|Cooperative Guidance Law against Highly Maneuvering Target with Dynamic Surrounding Attack
DOAJ | 2021
|Fixed-Time Convergence Cooperative Guidance Law Against Maneuvering Target
Springer Verlag | 2021
|Near optimal 3-D guidance against a maneuvering target
AIAA | 1989
|