论文部分内容阅读
针对木星-火星-航天器系统,根据欧拉-拉格朗日方程建立了航天器的动力学方程,并通过数值模拟,研究了系统的零速度曲面和Jacobi常数的几何结构的关系,设计了一条可用于多任务轨道的从火星至木星的转移轨道。
For the Jupiter-Mars-spacecraft system, the dynamics equations of the spacecraft are established according to Euler-Lagrange equations. The relationship between the zero-velocity surface of the system and the geometric structure of the Jacobi constant is studied by numerical simulation. A transitional trajectory from Mars to Jupiter that can be used for multitasking orbits.