Zobrazeno 1 - 2
of 2
pro vyhledávání: '"林敏杰"'
Publikováno v:
Tongxin xuebao, Vol , Pp 70-75 (1991)
Externí odkaz:
https://doaj.org/article/b50e7d835dd54380a8b56f5f27bd209a
Autor:
Lin, Miin-Jye, 林敏傑
85
Orbit integration for low orbiter is an extremely time consuming computation. In this study three methods are proposed to overcome this difficulty: the pred ict-pseudo correct method, the FFT evaluation of accelerations by parts, and t he PVM
Orbit integration for low orbiter is an extremely time consuming computation. In this study three methods are proposed to overcome this difficulty: the pred ict-pseudo correct method, the FFT evaluation of accelerations by parts, and t he PVM
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/63452265526181660660
