Finite-Thrust Trajectory Optimal of Earth Orbit Transfer with J2 Perturbation Considered by Homotopic Approach

被引：0

作者：

Huang An-yi ^{[1
]}

Zhang Zhi-bin ^{[1
]}

Li Heng-nian ^{[1
]}

机构：

[1] Xian Satellite Control Ctr, State Key Lab Astronaut Dynam, Xian 710043, Shaanxi, Peoples R China

来源：

2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2018年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Finite-thrust earth orbit transfer is studied with J2 perturbation considered in the dynamics. Firstly, the state equation of system is set up. Then based on minimum principle, the minimum conditions are readjusted. The whole solve process is then proposed. To reduce the difficulty in guessing of initial state values, method of extending the J2 step by step is introduced. Simulation result proved that the algorithm is practical and effective, which can be well applied in earth orbit transfers.

引用

页数：5

共 10 条

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