Feedback Linearisation for Nonlinear Vibration Problems

Feedback linearisation is a well-known technique in the controls community but has not been widely taken up in the vibrations community. It has the advantage of linearising nonlinear system models, thereby enabling the avoidance of the complicated mathematics associated with nonlinear problems. A particular and common class of problems is considered, where the nonlinearity is present in a system parameter and a formulation in terms of the usual second-order matrix differential equation is presented. The classical texts all cast the feedback linearisation problem in first-order form, requiring repeated differentiation of the output, usually presented in the Lie algebra notation. This becomes unnecessary when using second-order matrix equations of the problem class considered herein. Analysis is presented for the general multidegree of freedom system for those cases when a full set of sensors and actuators is available at every degree of freedom and when the number of sensors and actuators is fewer than the number of degrees of freedom. Adaptive feedback linearisation is used to address the problem of nonlinearity that is not known precisely. The theory is illustrated by means of a three-degree-of-freedom nonlinear aeroelastic model, with results demonstrating the effectiveness of the method in suppressing flutter.

[1]  Amir Poursamad,et al.  Adaptive feedback linearization control of antilock braking systems using neural networks , 2009 .

[2]  W. Marsden I and J , 2012 .

[3]  Derek P. Atherton,et al.  Stability of nonlinear systems , 1981 .

[4]  A. Isidori Nonlinear Control Systems , 1985 .

[5]  Charalampos P. Bechlioulis,et al.  Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance , 2008, IEEE Transactions on Automatic Control.

[6]  Andrew J. Kurdila,et al.  Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity , 1997 .

[7]  John E. Mottershead,et al.  Multiple-input active vibration control by partial pole placement using the method of receptances , 2013 .

[8]  Alireza Mohammad Shahri,et al.  Adaptive feedback linearizing control of nonholonomic wheeled mobile robots in presence of parametric and nonparametric uncertainties , 2011 .

[9]  A. Kurdila,et al.  Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity , 1997, 4th International Symposium on Fluid-Structure Interactions, Aeroelasticity, Flow-Induced Vibration and Noise: Volume III.

[10]  Miroslav Krstic,et al.  Control of Wing Rock Motion Using Adaptive Feedback Linearization , 1996 .

[11]  Jonathan E. Cooper,et al.  Introduction to Aircraft Aeroelasticity and Loads , 2007 .

[12]  Jonathan E. Cooper,et al.  Adaptive Feedback Linearisation and Control of a Flexible Aircraft Wing , 2014 .

[13]  Viet-Hung Dang,et al.  Partial feedback linearization control of a three-dimensional overhead crane , 2013 .

[14]  Thor I. Fossen,et al.  Adaptive feedback linearization applied to steering of ships , 1993 .

[15]  Aaas News,et al.  Book Reviews , 1893, Buffalo Medical and Surgical Journal.

[16]  A. Kurdila,et al.  Stability and Control of a Structurally Nonlinear Aeroelastic System , 1998 .