Fengyun-4 Attitude Control System Design and Its In-Flight Performance
Author:
Affiliation:
1. Beijing Institute of Control Engineering, 100094 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34226
Reference8 articles.
1. Guidance, navigation, and control performance for the GOES-R spacecraft
2. An Introduction to Himawari-8/9— Japan’s New-Generation Geostationary Meteorological Satellites
3. Attitude motion compensation for imager on Fengyun-4 geostationary meteorological satellite
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