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International Journal of Aerospace Engineering - Volume 2015 2015, Article ID 439815, 12 pages -

Research Article

State Key Laboratory of Virtual Reality Technology and Systems, Beihang University, Beijing 100091, China

College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received 4 August 2015; Revised 10 November 2015; Accepted 24 November 2015

Academic Editor: Paul Williams

Copyright © 2015 Bing Hua and Zhujun Shao. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


With radar and surface-to-air missiles posing an increasing threat to on-orbit spacecraft, low-observable satellites play an important role in low-thrust transfers. This paper presents the design for a low-thrust geostationary earth orbit GEO transfer control strategy which takes into consideration the low-observable constraint and discusses Earth shadow and perturbation. A control parameter optimization addresses the orbit transfer problem, and five thrust modes are used. Simulation results show that the method outlined in this paper is simple and feasible and results in reduced transfer time with a small amount of calculation. The method therefore offers a useful reference for low-thrust GEO transfer design.

Autor: Bing Hua and Zhujun Shao

Fuente: https://www.hindawi.com/


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