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    jsp.display-item.identifier=請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/38410

    题名: The analysis and synthesis of nonlinear three-dimensional guidance laws using phase plane methods in modified polar coordinate
    作者: 田豐;Tyan, Feng
    贡献者: 淡江大學航空太空工程學系
    关键词: 飛行動力學;飛行導引律;捕獲面積;極坐標Flight Dynamics;Navigation Guidance Law;Capture Area;Polar Coordinate
    日期: 2000-04
    上传时间: 2010-01-11 15:14:25 (UTC+8)
    摘要: In this paper, we presents the general three-dimensional guidance laws. With the aid of the modified polar coordinate, the expression of relative dynamics between target and missile becomes simple, and the constructed guidance law is intuitive and naive. Furthermore, a phase plane method is used to analyze the capture condition of the corresponding guidance law. The result is not restricted to time-invariant navigation constant. For a nonmaneuvering target or a maneuvering target but with known acceleration, it can be seen that only range rate divided by range and the rate of the magnitude of the unit vector along line of sight are related to the intercept condition.
    關聯: 第四屆海內外華人航天科技研討會論文集, 頁109-116
    显示于类别:[航空太空工程學系暨研究所] 會議論文





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