[1] BRAGG M B, HUTCHISON T,MERRET J,et al.Effect of ice accretion on aircraft flight dynamics:AIAA-2000-0360[R].Reston:AIAA,2000.
[2] POKHARIYAL D,BRAGG M B,HUTCHISON T,et al.Aircraft flight dynamics with simulated ice accretion:AIAA-2001-0541[R].Reston:AIAA,2001.
[3] 徐忠达,苏媛,曹义华.平尾积冰对飞机纵向气动参数的影响[J].航空学报,2013,34(7):1563-1571.XU Z D,SU Y,CAO Y H.Effects of tailplane icing on aircraft longitudinal aerodynamic parameters[J].Acta Aeronautica et Astronautica Sinica,2013,34(7):1563-1571(in Chinese).
[4] 张强,刘艳,高正红.结冰条件下的飞机飞行动力学仿真[J].飞行力学,2011,29(3):4-7.ZHANG Q,LIU Y,GAO Z H.Simulation of aircraft flight dynamics affected by ice accretion[J].Flight Dynamics,2011,29(3):4-7(in Chinese).
[5] 周莉,徐浩军,龚胜科,等.飞机结冰特性及防除冰技术研究[J].中国安全科学学报,2010,20(6):105-110.ZHOU L,XU H J,GONG S K,et al.Research of aircraft icing characteristics and anti-icing and de-icing technology[J].China Safety Science Journal,2010,20(6):105-110(in Chinese).
[6] 王海涛,毛玉坤.机翼结冰分析与防除冰系统设计验证[J].航空工程进展,2016,7(4):439-446.WANG H T,MAO Y K.Analysis of aircraft icing and design of anti-icing system[J].Advances in Aeronautical Science and Engineering,2016,7(4):439-446(in Chinese).
[7] 杜雁霞,李明,桂业伟,等.飞机结冰热力学行为研究综述[J].航空学报,2017,38(2):277-288.DU Y X,LI M,GUI Y W,et al.Review of themodynamic bahaviors in aircraft icing process[J].Acta Aeronautica et Astronautica Sinica,2017,38(2):277-288(in Chinese).
[8] FALKENA W,BORST C,MULDER J A.Investigation of pratical flight envelope protection systems for small aircraft:AIAA-2010-0711[R].Reston:AIAA,2010.
[9] ANSELL P J,BRAGG M B,KERHO M F.Envelope protection system using flag hinge moment measurements:AIAA-2010-4255[R].Reston:AIAA,2010.
[10] GURBACKI H M,BRAGG M B.Sending aircraft icing effects by flap hinge moment measurements:AIAA-99-3149[R].Reston:AIAA,1999.
[11] 徐彦军,林正,孙岩,等.基于H∞控制的飞机俯仰角控制系统设计[J].飞行力学,2010,28(6):24-27.XU Y J,LIN Z,SUN Y,et al.Design of aircraft pitching angle control system based on H∞ control[J].Flight Dynamics,2010,28(6):24-27(in Chinese).
[12] BRAGG M B,PERKINS W R,SARTER N B,et al.An interdisciplinary approach to inflight aircraft icing safety:AIAA-1998-0095[R].Reston:AIAA,1998.
[13] AYKAN R, HAJIYEV C,CALISKAN F.Aircraft icing detection,identification and reconfigurable control based on Kalman filtering and neral networks:AIAA-2005-6220[R].Reston:AIAA,2005.
[14] AYKAN R, HAJIYEV C,CALISKAN F.Kalman filter and neural network-based icing identification applied to A340 aircraft dynamics[J].Aircraft Engineering and Aerospace Technology,2005,77(1):23-33.
[15] 杜亮,洪冠新.结冰对飞机飞行包线影响分析及控制[J].飞行力学,2008,26(2):9-12.DU L,HONG G X.Analysis and control of icing effects on aircraft flight envelope[J].Flight Dynamics,2008,26(2):9-12(in Chinese).
[16] 王小龙,徐浩军,薛源,等.俯仰姿态保持模式下飞机结冰边界保护方法[J].航空动力学报,2016,31(9):2087-2094.WANG X L,XU H J,XUE Y,et al.Envelope protection method for pitch attitude holding mode under flight icing conditions[J].Journal of Aerospace Power,2016,31(9):2087-2094(in Chinese).
[17] 应思斌.飞机容冰飞行控制系统设计的理论与方法研究[D].上海:复旦大学,2010.YING S B.Study on the theory and methods of aircraft icing tolerant flight control system design[D].Shanghai:Fudan University,2010(in Chinese).
[18] 王晓燕,熊德琨.输入-输出非线性反馈线性化方法在飞控系统中的应用[J].南方冶金学院学报,2001,25(4):47-51.WANG X Y,XIONG D K.Input-output feedback linearization used in airplane control system[J].Journal of Southern Institute of Metallurgy,2001,25(4):47-51(in Chinese).
[19] 李大东,孙秀霞,董文瀚,等.基于线性化反馈的滑膜变结构重装空投纵向控制律设计[J].控制理论与应用,2013,30(1):54-60.LI D D,SUN X X,DONG W H,et al.Pitch control for flight in heavy-weight airdrop based on feedback linearization theory and variable-structure control[J].Control Theory and Applications,2013,30(1):54-60(in Chinese).
[20] BRAGG M B. Aerodynamics of supercooled-large-droplet ice accretions and the effect on aircraft control[C]//Proceedings of the FAA International Conference on Aircraft Inflight Icing.Washington,D.C.:FAA,1996:387-400.
[21] DETERS R W, DIMOCK G A,SELIG M S.Icing encounter flight simulator[J].Journal of Aircraft,2006,43(5):1528-1537.
[22] NELSON R C.Flight stability & automatic control[M].2nd ed.New York:McGraw-Hill Companies,1998:153-155. |