کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
5472332 | 1519916 | 2017 | 5 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Attitude motion compensation for imager on Fengyun-4 geostationary meteorological satellite
دانلود مقاله + سفارش ترجمه
دانلود مقاله ISI انگلیسی
رایگان برای ایرانیان
کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
چکیده انگلیسی
- An attitude motion compensation method for Chinese Fengyun-4 satellite is proposed.
- The method can counteract the line-of-sight deviation during attitude motion.
- The compensation is added to the instrument scanning control circuit and executed.
- An imaging test with the three-axis air-bearing physical simulator is proposed.
A compensation method is used in Chinese Fengyun-4 satellite to counteracting the line-of-sight influence by attitude motion during imaging. The method is acted on-board by adding the compensation amount to the instrument scanning control circuit. The mathematics simulation and the three-axis air-bearing test results show that the method works effectively.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 138, September 2017, Pages 290-294
Journal: Acta Astronautica - Volume 138, September 2017, Pages 290-294
نویسندگان
Wang Lyu, Shoulun Dai, Yaohai Dong, Yili Shen, Xiaozheng Song, Tianshu Wang,