利用自然进动实现圆轨道间的小推力转移
Low-Thrust Transfer Between Circular Orbits Using Natural Precession
摘要：
使用Edelbaum的平均动力学，加上由于第一纬向项的节点进动，制定了最小燃料低推力的圆形轨道之间的转移。极值分析表明，在常规情况下，最优转移由三个序列组成。最优控制问题的求解是通过一个由近似解得到的协态猜测的打靶法。
英文摘要：
The minimum-fuel low-thrust transfer between circular orbits is formulated using the Edelbaum's averaged dynamics with the addition of the nodal precession due to the first zonal term. The extremal analysis shows that an optimal transfer is composed of three sequences in the regular case. The optimal control problem is solved by a shooting method with a costate guess derived from an approximate solution.
机构、总结、中文摘要均由AI分析而来，可能存在错误，请以论文正文为准。
