@inproceedings{8b0694f8382e496c94c22d7d1554eecf,
title = "An Orbit Design Method for a Single Spacecraft to Visit Multiple Targets",
abstract = "In this paper, an orbit design method is presented to design a circle orbit for a single spacecraft without maneuvering to visit multiple targets with the same altitude. Based on the necessary condition of the flight time in circle orbit, one of the visit times can be solved when another visit time is determined. Then, an orbit design to visit three targets is translated into the minimum required velocity difference in the same position, and the Newton iteration method is utilized to find a high-precision result. Simulation results illustrate the effectiveness of the orbit design methods.",
keywords = "Circle Orbit, Multiple Targets Visit, Non-Maneuvering, Orbit Design Method",
author = "Zenan Zhong and Zhengxiang Sun and Songyan Wang and Tao Chao and Ming Yang",
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 = "10.1007/978-981-96-2208-5\_51",
language = "英语",
isbn = "9789819622078",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "536--545",
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 3",
address = "德国",
}