[1] WRIGHT J R,COOPER J E.飞机气动弹性力学及载荷导论[M].姚一龙,译.上海:上海交通大学出版社,2010:281-313. WRIGHT J R,COOPER J E.Introduction to aircraft aeroelasticity and loads[M].YAO Y L,translated.Shanghai:Shanghai Jiao Tong University Press,2010:281-313(in Chinese). [2] 毕莹.大展弦比飞机阵风减缓设计与试验研究[D].北京:北京航空航天大学,2017:1-10.BI Y.Control law and wind tunnel test about gust alleviation of high-aspect-ratio aircraft[D].Beijing:Beihang University,2017:1-10(in Chinese). [3] FULLER J R.Evolution of airplane gust loads design requirements[J].Journal of Aircraft,1995,32(2):235-246. [4] 杨俊斌,吴志刚,戴玉婷,等.飞翼布局飞机阵风减缓主动控制风洞试验[J].北京航空航天大学学报,2017,43(1):184-191.YANG J B,WU Z G,DAI Y T,et al.Wind tunnel test of gust alleviation active control for flying wing configuration aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2017,43(1):184-191(in Chinese). [5] LIU X,SUN Q,COOPER J E.LQG based model predictive control for gust alleviation[J].Aerospace Science and Technology,2017,71:499-509. [6] COOK R G,PALACIOS R,GOULART P.Robust gust alleviation and stabilization of very flexible aircraft[J].AIAA Journal,2013,51(2):330-340. [7] ALAM M,HROMCIK M,HANIS T.Active gust load alleviation system for flexible aircraft:Mixed feedforward/feedback approach[J].Aerospace Science and Technology,2015,41:122-133. [8] ZHAO Y H,YUE C Y,HU H Y.Gust load alleviation on a large transport airplane[J].Journal of Aircraft,2016,53(6):1932-1946. [9] 孙玉凯,张仁嘉,吴志刚,等.航模舵机的动态特性测试与系统辨识[J].北京航天航天大学学报,2020,46(2):294-303.SUN Y K,ZHANG R J,WU Z G,et al.Dynamical tests and system identification of small UAV actuators[J].Journal of Beijing University of Aeronautics and Astronaustics,2020,46(2):294-303(in Chinese). [10] 杨建忠,徐丹,杨士斌,等.考虑非线性因素的阵风减缓系统建模与仿真[J].飞行力学,2018,36(4):48-52.YANG J Z,XU D,YANG S B,et al.Modeling and simulation of gust alleviation system with system nonlinearity[J].Flight Dynamics,2018,36(4):48-52(in Chinese). [11] 黄伟,李芹,王志萍.增益和相位补偿的双模Smith预估控制算法[J].上海电力学院学报,2011,27(6):603-607.HUANG W,LI Q,WANG Z P.Research on dual-model Smith predictive control with gain and phrase compensation[J].Journal of Shanghai University of Electric Power,2011,27(6):603-607(in Chinese). [12] 唐功友.时滞系统的降维状态预测器及预测控制器设计[J].控制理论与应用,2004,21(2):295-298.TANG G Y.Design of reduced-order predictive state observer and predictive controller for systems with time-delay[J].Control Theory & Applications,2004,21(2):295-298(in Chinese). [13] 唐功友,雷靖,孙亮.控制时滞系统基于观测器的最优扰动抑制[J].控制理论与应用,2009,26(2):209-214.TANG G Y,LEI J,SUN L.Observer-based optimal disturbance-rejection for linear systems with time-delay in control action[J].Control Theory & Applications,2009,26(2):209-214(in Chinese). [14] MATEJICKOVA K,BAKOSOVA M.Robust PI controller desing for a time-delay process[C]//Proceedings of 2013 International Conference on Process Control.Piscataway:IEEE Press,2013:480-485. [15] KIM I H,JEONG G J,SON Y I.An adaptive output feedback control for time-delay systems with input disturbance[C]//Proceedings of ICROS-SICE International Joint Coferenece 2009.Piscataway:IEEE Press,2009:1742-1746. [16] NATORI K.A design method of time-delay systems with communication disturbance observer by using Padé approximation[C]//Proceedings of 2012 12th IEEE International Workshop on Advanced Motion.Piscataway:IEEE Press,2012:1-6. [17] QIAN W M,HUANG R,HU H Y,et al.Active flutter suppression of a multiple-actuated-wing wind tunnel model[J].Chinese Journal of Aeronautics,2014,27(6):1451-1460. [18] 吕志民,周茂林.使用Padé近似式处理数字控制系统中的纯滞后[J].中山大学学报,2001,40(1):114-115.LÜ Z M,ZHOU M L.Manipulation of the pure time delay in digital control system applying Padé approximation[J].Acta Scientiarum Naturalium University Sunyatseni,2001,40(1):114-115(in Chinese). [19] DORF R C,BISHOP R H.Modern control systems[M].12th ed.Upper Saddle River:Prentice Hall,2010:835-908. [20] OGATA K.Modern control engineering[M].5th ed.Upper Saddle River:Prentice Hall,2010:751-805. [21] 黄超.柔性飞翼飞机颤振主动抑制系统建模、设计与验证[D].北京:北京航空航天大学,2018:95-99.HUANG C.Modeling,design,and verification of active flutter suppression system acting on flexible flying-wing aircraft[D].Beijing:Beihang University,2018:95-99(in Chinese). [22] 熊纲,杨超.平衡截断法在气动伺服弹性系统模型降阶中的应用[J].航空学报,2001,22(2):168-170.XIONG G,YANG C.Application of balanced truncation method on aeroservoelastic model reduction[J].Acta Aeronautic et Astronautica Sinica,2001,22(2):168-170(in Chinese). [23] 尤明,宗群,曾凡琳,等.基于平衡截断方法的高超声速飞行器模型降阶[J].控制理论与应用,2014,31(6):795-800.YOU M,ZONG Q,ZENG F L,et al.Model order reduction for hypersonic vehicle based on balanced truncate method[J].Control Theory & Applications,2014,31(6):795-800(in Chinese). [24] 朱盟,曹国武,张志伟,等.基于Levy法的气动舵机系统辨识[J].弹箭与制导学报,2011,31(6):69-72.ZHU M,CAO G W,ZHANG Z W,et al.The system identification of pneumatic actuator based on Levy method[J].Journal of Projectiles,Rockets,Missiles and Guidance,2011,31(6):69-72(in Chinese). [25] KARPEL M,MOULIN B.Dynamic response of aeroservoelastic systems to gust exicitation[J].Journal of Aircraft,2005,42(5):1264-1272. [26] 肖叶伦,金长江.大气扰动中的飞行原理[M].北京:国防工业出版社,1993:116-181.XIAO Y L,JIN C J.Flight principle in atmosphere disturbance[M].Beijing:National Defense Industry Press,1993:116-181(in Chinese). [27] LEHTOMAKI N,SANDELL N,ATHANS M.Robustness results in linear-quadratic Gaussian based multivariable control designs[J].IEEE Transactions on Automatic Control,1981,26(2):75-93. |