非线性相对运动方程的分析解

Analytic Solution of the Nonlinear Equation of Relative Motion with Small Constant Thrust

阐述追踪航天器相对目标航天器的运动方程的建立 ,以线性相对运动方程分析解为基础 ,推导出非线性相对运动方程分析解 ,这里目标航天器沿一般椭圆轨道 (包括圆 )运动 。

Accurate equations of the relative motion are discussed,and analytic solutions of the linear equations are derived,based on analytic solutions of the linear equations,where the target vehicle moves on an elliptic orbit and the chaser vehicle is acted by small constant thrust.