摘要
With the rapid development of hypersonic vehicle technology, the research on defense approach of the hypersonic weapons is constantly deepening. A lot of guidance law researchers made their efforts to tackle with the problem of high speed, active large scale maneuverability of the hypersonic targets. In this paper, this interception problem is defined as a typical differential game, and the adaptive dynamic programming method is used to solve the Nash equilibrium Solution of the nonlinear continuous time System. The numerical Simulation of Matlab is provided to validate the effectiveness of the proposed guidance law. The result shows that the differential game guidance law based on adaptive dynamic programming is more robust than the baseline method- and can obtain higher interception aecuraey.
投稿的翻译标题 | Differential Game Guidance Law Based on Adaptive Dynamic Programming for the Interception of Hypersonic Targets |
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源语言 | 繁体中文 |
页(从-至) | 796-802 and 826 |
期刊 | Advances in Aeronautical Science and Engineering |
卷 | 11 |
期 | 6 |
DOI | |
出版状态 | 已出版 - 12月 2020 |
关键词
- Nash equilibrium Solution
- adaptive dynamic programming
- anti-hypersonic weapon
- differential game
- interception guidance law