@inproceedings{b65bc804a6dc47e891fdfe2e3e03f9ae,
title = "Impulsive relative hovering of space plane and trajectory safety analysis",
abstract = "The space plane relative hovering and trajectory safety analysis methods on the need of no-orbit servicing are presented in this paper. The expressions of the relative hovering dynamics are based on state transition matrix, which are uniformly valid for all elliptic reference orbits as well as the circular one. The impulsive maneuvers schemes provide convenience for the orbital maneuvering system of space plane. Based on the collision probabillty calculation, the analysis method of hovering trajectory safety is addressed to identify the risk of hovering maneuer, especially for the short-range and long-term relative hovering. The collision avoidance and hovering reconfiguration methods are introduced in this article to reduce the risk of collision and improve the accuracy of hovering. The numerical examples demonstrate the good performance of the methodology introduced in this work.",
author = "Bo Cheng and Jianping Yuan and Weihua Ma and Yingjing Qian",
note = "Publisher Copyright: {\textcopyright} 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 ; Conference date: 06-03-2017 Through 09-03-2017",
year = "2017",
doi = "10.2514/6.2017-2172",
language = "英语",
isbn = "9781624104633",
series = "21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017",
}