@inproceedings{1460d4560a154f4b9e2404f03d2c6922,
title = "Formation Flying and Transfer Orbit Analysis for LISA",
abstract = "LISA is a space-borne gravitational wave observatory. Gravitational waves detection in space requires the design of a suitable formation flying config-uration that provides a stable environment for detection. Based on LISA, this paper studies how trailing angle affects the configuration and transfer orbit in a more comprehensive way. The simulation results demonstrate that an initial trailing angle ranging from 18° to 23° ensures a stable configuration for LISA. A smaller initial angle facilitates launch but results in an unstable configuration. Conversely, selecting a larger initial trailing angle necessitates a larger maneuvering velocity increment but offers a more stable configuration.",
keywords = "Heliocentric formation flying configuration, LISA, Trailing angle, Velocity increment",
author = "Zhuo Li and Huixiang Ling and Tao Nie and Xiao Zhao and Qingzhong Gan",
note = "Publisher Copyright: {\textcopyright} The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.; International Conference on Guidance, Navigation and Control, ICGNC 2024 ; Conference date: 09-08-2024 Through 11-08-2024",
year = "2025",
doi = "10.1007/978-981-96-2228-3\_57",
language = "English",
isbn = "9789819622276",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "611--618",
editor = "Liang Yan and Haibin Duan and Yimin Deng",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 8",
address = "Germany",
}