Pulsar and Magnetar Navigation with Fermi/GBM and GECAM

The determination of the absolute and relative position of a spacecraft is critical for its operation, observations, data analysis, scientific studies, as well as deep-space exploration in general. A spacecraft that can determine its own absolute position autonomously may perform better than those t...

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Bibliographic Details
Main Authors: Xi-Hong Luo, Shuo Xiao, Shi-Jie Zheng, Ming-Yu Ge, You-Li Tuo, Shao-Lin Xiong, Shuang-Nan Zhang, Fang-Jun Lu, Yue Huang, Cheng Yang, Qi-Jun Zhi, Li-Ming Song, Wen-Xi Peng, Xiang-Yang Wen, Xin-Qiao Li, Zheng-Hua An, Jin Wang, Ping Wang, Ce Cai, Cheng-Kui Li, Xiao-Bo Li, Fan Zhang, Ai-Jun Dong, Wei Xie, Jian-Chao Feng, Qing-Bo Ma, Hua Wang De, Lun-Hua Shang, Xin Xu, Meng-Xuan Zhang, Zi-Ping Dong, Shi-Jun Dang
Format: Article
Language:English
Published: IOP Publishing 2023-01-01
Series:The Astrophysical Journal Supplement Series
Subjects:
Online Access:https://doi.org/10.3847/1538-4365/acc79d
Description
Summary:The determination of the absolute and relative position of a spacecraft is critical for its operation, observations, data analysis, scientific studies, as well as deep-space exploration in general. A spacecraft that can determine its own absolute position autonomously may perform better than those that must rely on transmission solutions. In this work, we report an absolute navigation accuracy of ∼20 km using 16 day Crab pulsar data observed with Fermi’s Gamma-ray Burst Monitor (GBM). In addition, we propose a new method with the inverse process of the triangulation for joint navigation using repeated bursts like those from the magnetar SGR J1935+2154 observed by the Gravitational-wave High-energy Electromagnetic Counterpart All-sky Monitor and GBM.
ISSN:0067-0049