@inproceedings{2db2337439f946eda7422bb32a333b56,
title = "New spacecraft forced fly-around formations design based on relative orbit elements",
abstract = "In order to meet the needs of spacecraft on-orbit service missions to fly-around technology, we have investigated the control of forced spacecraft fly-around in this paper. The paper introduces the relative orbit elements proposed by Lovell, which are the basis of our investigation about the fly-around. The three flyaround formations, the bi-elliptic, the teardrop and the bi-teardrop, are introduced. Based on the relative orbital elements, the pulse control strategy of each fly-around formation is solved and we simulated the three configurations. Also we introduce the theory of solving the relative motion trajectory and make an example of the reconstruction about the fly-around configuration. Finally, the pulse size and fly-around distance of the three fly-around configurations are prepared and we complete some explorations on the optimization of pulse control strategies.",
author = "Xi Jiaqi and Zhang Ran and Han Chao",
note = "Publisher Copyright: {\textcopyright} 2018 KASHYAP.; 4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 ; Conference date: 21-05-2018 Through 23-05-2018",
year = "2018",
language = "英语",
isbn = "9780877036531",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "67--86",
editor = "Jeng-Shing Chern and Ya-Zhong Luo and Xiao-Qian Chen and Lei Chen",
booktitle = "Dynamics and Control of Space Systems",
}