Control of Rotorcraft Retreating Blade Stall Using Air-Jet Vortex Generators
نویسندگان
چکیده
منابع مشابه
Backstepping Designs for Jet Engine Stall and Surge Control
M. Krstic Dept. Mechanical Engr. University of Maryland College Park, MD 20742 J. M. Protz and J. D. Paduano Massachusetts Institute of Technology Cambridge, MA 02139 P. V. Kokotovic Dept. Electr. & Comp. Engr. University of California Santa Barbara, CA 93106 Abstract. A new systematic method for nonlinear control design|backstepping|is applied to low-order compression system models. Backsteppi...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 2006
ISSN: 0021-8669,1533-3868
DOI: 10.2514/1.18333