@inproceedings{173221074c7d43d0af5c2c71a8d72a09,
title = "DYNAMIC ANALYSIS OF A THREE-BODY TETHERED SATELLITE SYSTEM WITH DEPLOYMENT/RETRIEVAL IN THREE-DIMENSIONAL",
abstract = "This paper investigates the model and nonlinear dynamic characteristic of a three-body tethered satellite system in three-dimensional. A novel dynamic model was derived by applying Newton{\textquoteright}s Second Law and a comparison of this new model with other model formed by the Lagrange equation verified the effectivity of the proposed model. Owing to the physical meaning of each part of the dynamics equations, the out-plane dynamic performances of the system were investigated and analysed. Results show that parts of libration energy deliver from out-plane to in-plane, while libration energy do not transfer from in-plane motion to out-plane motion. Finally, a deployment strategy was proposed to suppress the libration motion during the phase of tether expansion. Furthermore, simulation results were presented to show effectiveness and efficiency of the method.",
keywords = "Deployment strategy, Dynamic analysis, Libration motion, Three-body tethered satellite system",
author = "Teng He and Zhanxia Zhu and Luo Jianjun and Jianping Yuan",
note = "Publisher Copyright: Copyright {\textcopyright} 2021 by the International Astronautical Federation (IAF). All rights reserved.; 19th IAA Symposium on Visions and Strategies 2021 at the 72nd International Astronautical Congress, IAC 2021 ; Conference date: 25-10-2021 Through 29-10-2021",
year = "2021",
language = "英语",
series = "Proceedings of the International Astronautical Congress, IAC",
publisher = "International Astronautical Federation, IAF",
booktitle = "19th IAA Symposium on Visions and Strategies 2021 - Held at the 72nd International Astronautical Congress, IAC 2021",
}