A STUDY OF LOW-THRUST TRAJECTORIES FOR LOW ORBIT MULTIPLE CUBESAT MISSIONS

被引：0

作者：

Ghosh, Alexander ^{[1
]}

Coverstone, Victoria ^{[1
]}

机构：

[1] Univ Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA

来源：

SPACEFLIGHT MECHANICS 2010, PTS I-III | 2010年 / 136卷

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：

This work discusses the usage of a low-thrust micro-cavity discharge thruster on 3 kg cubesats. Based on a case study of a two-satellite system, the required trajectories, and control use is determined to allow the cubesats to recover from disturbances, and extended their usable lifetime by a factor of at least 10. The approach uses a direct transcription method that employs multiple-shooting of a 4th order Runge-Kutta forward-integration of the state and control defects. It also lays the groundwork for future study into problems regarding cubesat formation phasing with larger numbers of spacecraft.

引用

页码：1117 / 1133

页数：17

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