A robust nonlinear output feedback control method for limit cycle oscillation suppression using synthetic jet actuators
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Aerospace Science and Technology
سال: 2017
ISSN: 1270-9638
DOI: 10.1016/j.ast.2016.12.030