@inproceedings{44097f0d2cb142f68b4bd11a22bede26,
title = "Reachable domain for satellite with continuous low-thrust based on the two body model",
abstract = "The reachable domain (RD) for satellite with continuous low-thrust that initially orbits Earth in a circular orbit is investigated. The standard Two Body model is employed. Establishing a frame of reference moving along with the RD, we determine the boundary of the RD by looking for the largest displacement the satellite may accomplish in an arbitrarily chosen spatial direction. Thus the RD solving problem is converted into a series of finite-time optimal control problems which can be solved by a Newton's shooting method. By traversing all the spatial attitude angles we finally obtain the numerical solution of the RD.",
author = "Haoran Gong and Shengping Gong",
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 = "1845--1850",
editor = "Jeng-Shing Chern and Ya-Zhong Luo and Xiao-Qian Chen and Lei Chen",
booktitle = "Dynamics and Control of Space Systems",
}