Feedback Gain Sensitivities of Closed-Loop Modal Parameters of Controlled Structures

作者: James A. Fabunmi

DOI: 10.2514/3.21097

关键词: EngineeringPlantDisplacement (vector)Symbolic computationOptimal controlCantileverControl theorySensitivity (control systems)ActuatorModal

摘要: Computer algebra (MACSYMA) has been used to derive the characteristic polynomials that determine closed-loop frequencies and damping coefficients of output-feedba ck controlled structures. These expressions show explicitly how locations actuator/sensor pairs displacement velocity feedback gains influence parameters system modes. For lightly coupled modes, simple relations are obtained between modal coordinates sensor/actuator as well gains. Using example a cantilevered uniform beam by single pair, numerical results illustrate sensitivity closedloop placement pair Such help answer questions about optimal sensor/actuat or for active control flexible structure.

参考文章(16)
Leonard Meirovitch, Control of Distributed Structures Springer Berlin Heidelberg. pp. 195- 212 ,(1988) , 10.1007/978-3-642-83376-2_9
P. J. Lynch, Siva S. Banda, Active Control for Vibration Damping Springer, Berlin, Heidelberg. pp. 239- 261 ,(1988) , 10.1007/978-3-642-83376-2_11
Applications of computer algebra Kluwer Academic Publishers. ,(1985) , 10.1007/978-1-4684-6888-5
Jer-Nan Juang, Minh Phan, Robust controller designs for second-order dynamic systems - A virtual passive approach Journal of Guidance Control and Dynamics. ,vol. 15, pp. 1192- 1198 ,(1992) , 10.2514/3.20968
G. HORNER, J. WALZ, A design technique for determining actuator gains in spacecraft vibration control 26th Structures, Structural Dynamics, and Materials Conference. ,(1985) , 10.2514/6.1985-628
R.A. Burdisso, C.R. Fuller, Eigenproperties of Feedforward Controlled Flexible Structures Journal of Intelligent Material Systems and Structures. ,vol. 2, pp. 494- 507 ,(1991) , 10.1177/1045389X9100200405