摘要
Although attitude stabilization technology reduces the lateral dispersion of long-range rockets effectively, their range dispersion is still not satisfactory. A range correction for the attitude stabilized rocket is necessary. A key point of the range correction is accurate range prediction. In this paper, some prediction methods were proposed and Monte Carlo method was adopted to analyze their efficiency.
源语言 | 英语 |
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页(从-至) | 155-158 |
页数 | 4 |
期刊 | Binggong Xuebao/Acta Armamentarii |
卷 | 26 |
期 | 2 |
出版状态 | 已出版 - 3月 2005 |