Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion
نویسندگان
چکیده
منابع مشابه
-Optimal Gust Load Alleviation for a Flexible Aircraft
+2 (LQG), weighted-+2 and +∞ techniques are used to establish a nominal performance baseline for the vertical acceleration control of a B-52 aircraft model with flexibilities. The aircraft is assumed to be subjected to severe wind gusts causing undesirable vertical motion. The purpose of the controllers is to reduce the transient peak loads on the airplane caused by the gusts. Our designs accou...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2019
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.g003980