Bifurcation Stabilization withApplications in Jet Engine Control
نویسندگان
چکیده
Local output feedback stabilization with smooth nonlinear controllers is studied for parameterized nonlinear systems of which the linearized system possesses multiple pairs of imaginary eigen-values, and the bifurcated solution is unstable at the critical value of the parameter. Necessary and suucient conditions are sought for stabilization of such nonlinear bifurcated systems based on the projection method 16] and Lyapunov method 11]. The result was applied to axial ow compressors which are the essential part of jet engines. It is shown that the feedback control law proposed in 13] admits stabilizing property for axial ow compressors at the critical operating point.
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