摘要
This paper proposes a method for maneuvering a single air-to-air missile carrier. The equations were derived to indicate how the missile carrier should be maneuvered as to be in a favorable position for attacking the multi-targets treated as a single target. Numerical simulation shows that this method is simple and practicable, it can be used both in multitargets and single target conditions.
源语言 | 英语 |
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页(从-至) | 273-277 |
页数 | 5 |
期刊 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
卷 | 15 |
期 | 2 |
出版状态 | 已出版 - 1997 |