Fengyun-4 Attitude Control System Design and Its In-Flight Performance
| العنوان: | Fengyun-4 Attitude Control System Design and Its In-Flight Performance |
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| المؤلفون: | Liu Yiwu, Wang Kai, Tang Liang, Chen Shoulei |
| المصدر: | Journal of Spacecraft and Rockets. 56:200-210 |
| بيانات النشر: | American Institute of Aeronautics and Astronautics (AIAA), 2019. |
| سنة النشر: | 2019 |
| مصطلحات موضوعية: | Attitude control system, Meteorology, Computer science, Launched, Feed forward, Aerospace Engineering, Gyroscope, Orbital inclination, law.invention, Attitude control, Space and Planetary Science, law, Geostationary orbit, Meteorological satellite |
| الوصف: | Fengyun-4, launched on 11 December 2016, is a second-generation geostationary meteorological satellite that employs a three-axis-stabilized attitude control strategy with a zero-momentum state. Thi... |
| تدمد: | 1533-6794 0022-4650 |
| URL الوصول: | https://explore.openaire.eu/search/publication?articleId=doi_________::37e130eeb4e68255fb4fd046ad213c36 https://doi.org/10.2514/1.a34226 |
| رقم الأكسشن: | edsair.doi...........37e130eeb4e68255fb4fd046ad213c36 |
| قاعدة البيانات: | OpenAIRE |
| تدمد: | 15336794 00224650 |
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