Periodic Trajectory of Relative Motion Controlled by Constant Thrust

被引：0

作者：

Bai, Shengzhou ^{[1
]}

Han, Chao ^{[1
]}

Wang, Xiaohui ^{[1
]}

Sun, Xiucong ^{[1
]}

Zang, Jie ^{[2
]}

机构：

[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China

[2] China Acad Space Technol, Inst Spacecraft Syst Engn, Beijing 100094, Peoples R China

来源：

2019 THE 10TH ASIA CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ACMAE 2019) | 2020年 / 1510卷

基金：

北京市自然科学基金; 中国国家自然科学基金;

关键词：

SPACECRAFT;

D O I：

10.1088/1742-6596/1510/1/012024

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Formation flying has received widespread attention in recent years. However, the conventional control approaches require high demand for engine. To deal with this problem, the relative periodic trajectory can be achieved by multiple two-section constant thrust control proposed in this study. Firstly, the concept of the constant thrust control is presented. Furthermore, the strategy is presented to guarantees periodic trajectory considering J2 perturbation. Simulations are conducted to demonstrate the efficacy of the method. The proposed control approach is applied for engineering applications.

引用

页数：6

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