Finite-time attitude tracking control design for reusable launch vehicle in reentry phase based on disturbance observer
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Advances in Mechanical Engineering
سال: 2017
ISSN: 1687-8140,1687-8140
DOI: 10.1177/1687814017744077