@inproceedings{026b76d010ad4242bc632cfb2b71202b,
title = "A Low-thrust Spacecraft Propulsion Technology and Its Orbit Transfer Application",
abstract = "For the propulsion technology and orbit transfer control of low-thrust spacecraft, the previous traditional methods and technologies are relatively expensive and cannot guarantee the optimal solution. This paper proposes a new solution method for the low-thrust spacecraft propulsion technology and orbit transfer design, which can optimize the propulsion and orbit transfer flight of low-thrust spacecraft. Theoretical design shows that this method can quickly obtain the optimal analytical solution, and has good optimization effects on the propulsion and orbit transfer of low-thrust spacecraft.",
keywords = "electric propulsion technology, Low-thrust spacecraft, optimal control, orbit transfer",
author = "Shuo Han and Bo Mo and Wenli Li and Bo Jin",
note = "Publisher Copyright: {\textcopyright} 2024 Technical Committee on Control Theory, Chinese Association of Automation.; 43rd Chinese Control Conference, CCC 2024 ; Conference date: 28-07-2024 Through 31-07-2024",
year = "2024",
doi = "10.23919/CCC63176.2024.10661584",
language = "English",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3761--3766",
editor = "Jing Na and Jian Sun",
booktitle = "Proceedings of the 43rd Chinese Control Conference, CCC 2024",
address = "United States",
}