[1] THOMPSON G O,KASS G J.Active flutter suppression-An emerging technology[J].Journal of Aircraft,1972,9(3):230-235.
[2] MUKHOPADHYAY V.Flutter suppression digital control law design and testing for the AFW wind-tunnel model:AIAA-1992-2095[R].Reston:AIAA,1992.
[3] NISSIM E.Reduction of aerodynamic augmented states in active flutter suppression systems[J].Journal of Aircraft,1991,28(1):82-93.
[4] MAHESH J K,STONE C R,GARRARD W L,et al.Control law synthesis for flutter suppression using linear quadratic Gaussian theory[J].Journal of Guidance,Control,and Dynamics,1981,4(4):415-422.
[5] 吴志刚,杨超.主动气动弹性机的颤振主动抑制与阵风减缓研究[J].机械强度,2003,25(1):32-35.WU Z G,YANG C.Investigation on active flutter suppression and gust alleviation for an active aeroelastic wing[J].Journal of Mechanical Strength,2003,25(1):32-35(in Chinese).
[6] NA S,LIBRESCU L,MARZOCCA P,et al.Aeroelastic response of flapped wing systems using robust estimation methodology:AIAA-2004-1673[R].Reston:AIAA,2004.
[7] KIM K W,LEE B,NA S,et al.Comparative analysis of control performances applied to a 3-DOFs nonlinear supersonic lifting surface:AIAA-2008-1724[R].Reston:AIAA,2008.
[8] LEE K W,SINGH S N.Robust higher-order sliding-mode finite-time control of aeroelastic systems[J].Journal of Guidance,Control,and Dynamics,2014,37(5):1664-1670.
[9] ZHANG H Y,SHI Z K.Variable structure control of catastrophic course in airdropping heavy cargo[J].Chinese Journal of Aeronautics,2009,22(5):520-527.
[10] 宋晨,吴志刚,杨超.二元机翼滑模变结构控制颤振主动抑制[J].北京航空航天大学学报,2010,36(11):1400-1403.SONG C,WU Z G,YANG C.Sliding mode variable structure control of flutter suppression for a two-dimensional wing[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(11):1400-1403(in Chinese).
[11] YANG C,SONG C,WU Z G,et al.Application of output feedback sliding mode control to active flutter suppression of two-dimensional airfoil[J].Science China:Technological Sciences,2010,53(5):1338-1348.
[12] SONG C,WU Z G,YANG C.Active flutter suppression of a two-dimensional airfoil based on sliding mode control method[C]//The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics,Harbin,2010.
[13] EDWARDS C,SPURGEON S K.Sliding mode control:Theory and applications[M].London:Taylor & Francis,1998.
[14] 杨超,吴志刚,万志强,等.飞行器气动弹性原理[M].北京:北京航空航天大学出版社,2011.YANG C,WU Z G,WAN Z Q,et al.Principles of aeroelasticity for air vehicles[M].Beijing:Beihang University Press,2011 (in Chinese).
[15] YURKOVICH R.Status of unsteady aerodynamic prediction for flutter of high-performance aircraft[J].Journal of Aircraft,2003,40(5):832-842.
[16] 陈磊,吴志刚,杨超,等.多控制面机翼阵风减缓主动控制与风洞试验验证[J].航空学报,2009,30(12):2250-2256.CHEN L,WU Z G,YANG C,et al.Active control and wind tunnel test verification of multi-control surface wing for gust alleviation[J].Acta Aeronoutica et Astronautica Sinica,2009,30(12):2250-2256(in Chinese).
[17] 宋晨,杨超,吴志刚.3种气动弹性状态空间建模方法的对比[J].航空学报,2007,28(Sup.):S81-S86.SONG C,YANG C,WU Z G.Comparison of three aeroelastic state-space modeling methods[J].Acta Aeronoutica et Astronautica Sinica,2007,28(Sup.):S81-S86(in Chinese).
[18] 吴敏,桂卫华,何勇.现代鲁棒控制[M].2版.长沙:中南大学出版社,2006.WU M,GUI W H,HE Y.Modern robust control[M].2nd ed.Changsha:Central South University Press,2006(in Chinese). |