Abstract
This article considers the problem of optimal guidance laws for cooperative attack of multiple missiles based on the optimal control theory. New guidance laws are presented such that multiple missiles attack a single target simultaneously. Simulation results show the effectiveness of the proposed algorithms.
| Original language | English |
|---|---|
| Pages (from-to) | 1063-1070 |
| Number of pages | 8 |
| Journal | International Journal of Control |
| Volume | 85 |
| Issue number | 8 |
| DOIs | |
| Publication status | Published - 1 Aug 2012 |
Keywords
- hamiltonian
- many-to-one guidance
- optimal control theory
- optimal guidance law
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Sun, X., & Xia, Y. (2012). Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory. International Journal of Control, 85(8), 1063-1070. https://doi.org/10.1080/00207179.2012.675519