Active flutter suppression for two-dimensional airfoil based on improved SDRE nonlinear robust control

GOU Yi-yong, LI Hong-bo, DONG Xin-min,YANG Ren-nong,ZUO Ren-wei

Journal of Vibration and Shock ›› 2017, Vol. 36 ›› Issue (10) : 149-153.

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PDF(998 KB)
Journal of Vibration and Shock ›› 2017, Vol. 36 ›› Issue (10) : 149-153.

Active flutter suppression for two-dimensional airfoil based on improved SDRE nonlinear robust control

  • GOU Yi-yong, LI Hong-bo, DONG Xin-min, YANG Ren-nong ,ZUO Ren-wei
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Abstract

In order to achieve active flutter suppression of a two-dimensional airfoil, an improved state-dependent Riccati equation (SDRE) nonlinear robust control law is proposed based on Lyapunov stability theory. The model of a two-dimensional airfoil with leading- and trailing-edge control surfaces are described in state space, and then this model is transformed into a form which input matrix   is full row rank matrix. The problem that SDRE nonlinear control method can’t be directly applied to active flutter suppression is solved. The simulation results are presented, which show the closed-loop system reaches to stability quickly under the impact of wind gust even if there is a hard constraint on the control input and flutter suppression is accomplished effectively. In addition, adjusting the weighting parameters   and  can decrease control inputs. 
 

Key words

two-dimensional airfoil / nonlinear robust control / flutter / state-dependent Riccati equation

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GOU Yi-yong, LI Hong-bo, DONG Xin-min,YANG Ren-nong,ZUO Ren-wei. Active flutter suppression for two-dimensional airfoil based on improved SDRE nonlinear robust control[J]. Journal of Vibration and Shock, 2017, 36(10): 149-153

References

[1] Mukhopadhyay V. Historical perspective on analysis and control of aeroelastic responses[J]. Journal of Guidance, Control, and Dynamics, 2003, 26(5): 673–684.
[2] Xiang J W, YanY J, LiDaochun. Recent advance in nonlinear aeroelastic analysis and control of the aircraft[J]. Chinese Journal of Aeronautics, 2014, 27(1): 12-22.
[3] O’Neil T, Strganac T W. Aeroelastic response of a rigid wing supported by nonlinear springs[J]. Journal of Aircraft, 1998, 35(4): 616-622.
[4] M Cassaro, M Battipede, PMarzocca, A.Behal. Comparison of adaptive control architectures for flutter suppression[J].Journal of Guidance, Control, and Dynamics, 2015, 38(2): 346-354.
[5] SahjendraN.Singh, WoosoonYim. State feedback control of an aeroelastic system with structural nonlinearity[J]. Aerospace Science and Technology, 2003, 7, 23-31.
[6] M. Tadi, State-dependent Riccati equation for control of aeroelastic flutter[J]. Journal of Guidance, Control, and Dynamics, 2003, 26(6): 914-917
[7] Platanitis G, Strganac T W. Suppression of control reversal using leading- and trailing-edge control surfaces[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(3): 452-460.
[8] Platanitis G., Strganac T W. Control of a nonlinear wing section using leading- and trailing-edge surfaces[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(1): 52–58.
[9] Lee K W, Singh S N. Control of a wing section using leading-and trailing-edge flaps by L1 adaptive feedback despite disturbances[C]. //51st AIAA Aerospace Sciences Meeting and Exhibit, 2013: 2013-1111.
[10] Wang Z, Behal A, Marzocca P. Model-free control design for Multi-Input Multi-Output aeroelastic system subject to external disturbance[J] Journal of Guidance, Control, and Dynamics, 2011, 34(2): 446–458.
[11] Kelly D, Hammett. Control of nonlinear systems Via the state feedback state-dependen Riccati equation techniques[D]. Edmond: engineering of the air force institute of technology air university , 1997
[12] Mori T, Derese A. A brief summary of the bounds on the solution of the algebraic matrix equations in control theory. Iternationl Journal of Control[J], 1984, 39(2):247-256.
[13] Ridgely D B, Banda S S. Introduction to Robust Multivariable Control[D]. AFWAL-TR-85-3102, USAF, 1986.
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