Rotating stall control in axial compressor subject to wheel speed transients

被引:5
|
作者
Buhr, CA [1 ]
Franchek, MA [1 ]
Fleeter, S [1 ]
机构
[1] Purdue Univ, Sch Mech Engn, W Lafayette, IN 47907 USA
关键词
D O I
10.2514/1.6272
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A gain-scheduled controller design methodology for rotating stall control in an axial flow compressor subject to wheel speed transients is presented. Linear robust controllers are designed for a family of flow coefficients in the spatial domain at specified discrete wheel speeds to. regulate nonaxisymmetric flow. The resulting family of controllers are then gain scheduled with respect to wheel speed in an effort to address the transient wheel speed condition. To validate the performance of the gain schedule control law, domains of attraction obtained from initial condition simulated responses of the nonlinear compressor model are used.
引用
收藏
页码:404 / 410
页数:7
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