An adaptive inverse control scheme for a synthetic jet actuator model

被引：20

作者：

Deb, D ^{[1
]}

Tao, G ^{[1
]}

Burkholder, JO ^{[1
]}

Smith, DR ^{[1
]}

机构：

[1] Univ Virginia, Dept Elect & Comp Engn, Charlottesville, VA 22904 USA

来源：

ACC: Proceedings of the 2005 American Control Conference, Vols 1-7 | 2005年

关键词：

actuator nonlinearity; adaptive inverse; parameter projection; stability and tracking; synthetic jets;

D O I：

10.1109/ACC.2005.1470367

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this paper, we develop an adaptive inverse compensation scheme for controlling the aerodynamic flow of a synthetic jet actuator on a dynamic aircraft system. An adaptive inverse is employed for cancelling the effect of the nonlinearity of the synthetic jet. A linear state feedback control law is used for controlling the aircraft dynamics. A linearly parametrized error model is derived for the nonlinear actuator model. A parameter projection adaptive law is used to ensure desired closed-loop stability and asymptotic tracking. An application of this adaptive compensation scheme to the control of a linear aircraft model with a synthetic jet actuator is studied and its effectiveness is verified by simulation results.

引用

页码：2646 / 2651

页数：6

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