Sliding Mode Attitude Control of Spacecraft Considering Angular Rate Constraints

التفاصيل البيبلوغرافية
العنوان: Sliding Mode Attitude Control of Spacecraft Considering Angular Rate Constraints
المؤلفون: Henzeh Leeghim, Seok-ho Jang, Min-young Kim
المصدر: Journal of the Korean Society for Aeronautical & Space Sciences. 49:129-138
بيانات النشر: The Korean Society for Aeronautical & Space Sciences, 2021.
سنة النشر: 2021
مصطلحات موضوعية: Attitude control, Spacecraft, Computer science, business.industry, Control theory, Mode (statistics), business, Sliding mode control
تدمد: 2287-6871
1225-1348
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::2682edb96783c178a1daab4ff48e8b7c
https://doi.org/10.5139/jksas.2021.49.2.129
رقم الأكسشن: edsair.doi...........2682edb96783c178a1daab4ff48e8b7c
قاعدة البيانات: OpenAIRE