Backstepping Designs for Jet Engine Stall and Surge Control
نویسندگان
چکیده
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. Backstepping achieves global asymptotic stability of both stall and surge in the presence of large uncertainties in the compressor model. Throughout our presentation, we explore the control design implications of the nonlinear equilibrium properties of compressors.
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