Please use this identifier to cite or link to this item: http://hdl.handle.net/11455/44136
標題: Development of three-dimensional aiming point guidance law
作者: Lin, Y.P.
林俊良
Tsao, L.P.
Lin, C.L.
關鍵字: missile
guidance
proportional navigation
aiming point guidance
proportional navigation
homing missiles
期刊/報告no:: International Journal of Systems Science, Volume 41, Issue 11, Page(s) 1353-1362.
摘要: A new aiming point guidance (APG) law in 3-dimensional space is derived analytically. The guidance law is capable of guiding the missile (interceptor) to a straight collision course with respect to the target. The missile turning rate command proportional to the error angle between the current missile heading and the predicted aim point is calculated based on the predicted target position. Performance of the APG law is numerically evaluated and compared with the proportional navigation guidance (PNG) law. The result of numerical simulation shows that the APG law is superior to the PNG law in terms of miss distance, time of interception and final stage missile turning rate demand.
URI: http://hdl.handle.net/11455/44136
ISSN: 0020-7721
文章連結: http://dx.doi.org/10.1080/00207720903260176
Appears in Collections:電機工程學系所

文件中的檔案:

取得全文請前往華藝線上圖書館



Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.