Influence of unstable dynamics on orbit determination with x-ray pulsar navigation

Yang Zhou, Mai Bando, Shinji Hokamoto, Panlong Wu

研究成果: 書籍/レポート タイプへの寄稿会議への寄与

抄録

This paper explores the influence of unstable dynamics on orbit determination. A halo orbit about the Earth-Moon L2 is considered to be the nominal orbit and the dynamics model is constructed based on the Earth-Moon circular restricted three body problem. X-ray pulsar navigation method is introduced for orbit determination that is performed by Kalman filter. Simulation results show that unstable manifold of halo orbit dominates the growth of orbit-determination error and the corresponding uncertainty. However, when the orbit-determination measurements are incorporated in, the results change and are greatly influenced by the characteristic of the X-ray pulse measurements.

本文言語英語
ホスト出版物のタイトルDynamics and Control of Space Systems
編集者Jeng-Shing Chern, Ya-Zhong Luo, Xiao-Qian Chen, Lei Chen
出版社Univelt Inc.
ページ1827-1843
ページ数17
ISBN(印刷版)9780877036531
出版ステータス出版済み - 2018
イベント4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 - Changsha, 中国
継続期間: 5月 21 20185月 23 2018

出版物シリーズ

名前Advances in the Astronautical Sciences
165
ISSN(印刷版)0065-3438

その他

その他4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018
国/地域中国
CityChangsha
Period5/21/185/23/18

!!!All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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