摘要
本文讨论了地面战术火箭主动段质心运动的变系数非线性常微分方程组的稳定性,并提出了火箭临界离轨速度的概念。
In this paper, we study the stability of the variable coefficient nonlinear ordinary differential equations that discribe the motion concerning the center of mass of a ground tactial rocket, in the active part of its orbit, and give the critical velocity in which the rocket is launched from its launcher.
出处
《陕西科技大学学报（自然科学版）》
1992年第1期89-92,共4页
Journal of Shaanxi University of Science & Technology
