摘要
考虑地球自转时,定量讨论了导弹在柯氏力作用下。
The relation among the deviation of landing point, latitude and emission angle is discussed considering the effect of Coriolis force on the guided missile.
出处
《唐山师范学院学报》
2001年第5期55-57,共3页
Journal of Tangshan Normal University
