摘要
轨道预定路径控制问题,其数学模型是一个非线性的半显式微分/代数方程(DAE)系统.本文运用一类隐式Runge-Kuta方法求解指标2的DAT系统。
The model equations of trajectory prescribed path control problems (TPPC) are a nonlinear semi explicit differential algebraic equation system. In this paper, we present methods for solving TPPC, discuss advantages and disadvantages of the methods in applications and give an example for illustration.
出处
《数学杂志》
CSCD
1997年第4期513-516,共4页
Journal of Mathematics
基金
国家自然科学基金
关键词
路径控制
飞行器模拟
TPPC问题
轨道形状
trajectory prescribed path control index 2 differential algebraic equation Runge Kutta methods.