Nonlinear Negative Stiffness Wingtip Spring Device for Gust Loads Alleviation
نویسندگان
چکیده
منابع مشابه
Adaptive Feedforward Control for Gust Loads Alleviation
Active control techniques for the gust loads alleviation/flutter suppression have been investigated extensively in the last decades to control the aeroelastic response, and improve the handling qualities of the aircraft. Nonadaptive feedback control algorithms such as classical single input single output techniques (Schmidt & Chen, 1986), linear quadratic regulator (LQR) theory (Mahesh et al., ...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 2017
ISSN: 0021-8669,1533-3868
DOI: 10.2514/1.c033887