[1]王咏梅.全球民用直升机市场研究与分析[J].江苏科技信息, 2020, 37(17):34-37
[2]杨婧, 詹月玫, 洪彬.世界军用直升机装备现状及发展规划[J].直升机技术, 2020, (3):68-72
[3]田翔, 沈亚娟, 马小艳.旋翼主动控制技术研究[J].中国科技信息, 2019, (3):37-44
[4]EDWARDS B D, COX C, BOOTH E R.Revolutionary Concepts for Helicopter Noise Reduction: SILENT Program: NASA/CR-2002-2111650[R]. National Aeronautics and Space Administration, Langley Research Center, 2002.
[5]KESSLER C.Active rotor control for helicopters: motivation and survey on higher harmonic control[J].CEAS Aeronautical Journal, 2011, 1(1):3-22
[6]冯剑波, 陆洋.直升机旋翼桨涡干扰噪声主动控制技术综述[J].噪声与振动控制, 2018, 38(3):1-9
[7]FRIEDMANN P.On-Blade Control of Rotor Vibration,Noise,and Performance: Just Around the Corner? The 33rd Alexander Nikolsky Honorary Lecture[J].Journal of the American Helicopter Society, 2014, 59(4):1-37
[8]KESSLER C.Active rotor control for helicopters: individual blade control and swashplateless rotor designs[J].CEAS Aeronautical Journal, 2011, 1(1):23-54
[9]DIETERICH O, RABOURDIN A, MAURICE J B, et al.Blue Pulse?: active rotor control by trailing edge flaps at airbus helicopters—New EC145 demonstrator and flight test results [C]//Proceedings of the 70th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Soc. International, 2014:679-702.
[10]王潇, 杨一凡, 张硕.直升机振动主动控制方法研究综述[J].电光与控制, 2024, 31(5):1-10
[11]BENT A A, HAGOOD N W.Piezoelectric Fiber Composites with Interdigitated Electrodes[J].Journal of Intelligent Material Systems and Structures, 1997, 8:903-919
[12]VAN D W B G, LIM J W, RIEMENSCHNEIDER J, et al.New smart twisting active rotor (STAR): pretest predictions[J].CEAS Aeronautical Journal, 2024, 15(3):721-750
[13]THAKKAR D, GANGULI R.Active Twist Control of Smart Helicopter Rotor - A Survey[J].Journal of Aerospace Sciences and Technologies, 2023, 57(4):429-448
[14]CHOPRA I.Review of State of Art of Smart Structures and Integrated Systems[J].AIAA Journal, 2002, 40(11):2145-2187
[15]WILBUR M L, WILKIE W K.Active-twist rotor control applications for UAVs[M]. Transformational Science and Technology for the Current and Future Force: World Scientific, 2006: 185-192.
[16]WILLIAM K W, ROBERT G B, JAMES W H, et al.Low-cost piezocomposite actuator for structural control applications[C]//Smart structures and materials 2000: industrial and commercial applications of smart structures technologies. SPIE, 2000, 3991: 323-334.
[17]HAMED Y S, KANDIL A, MACHADO J T.Utilizing Macro Fiber Composite to Control Rotating Blade Vibrations[J].Symmetry, 2020, 12(12):1984-
[18]PAWAR P M, JUNG S N.Single-crystal-material-based induced-shear actuation for vibration reduction of helicopters with composite rotor system[J].Smart Materials and Structures, 2008, 17(6):065009-
[19]PAWAR P M, JUNG S N.Active twist control methodology for vibration reduction of a helicopter with dissimilar rotor system[J].Smart Materials and Structures, 2009, 18(3):035013-
[20]JOHNSON W, UNITED S.Self-tuning regulators for multicyclic control of helicopter vibration[M]. Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982.
[21]RAKOTOMAMONJY T, VU B D.Identification and optimal control methodology for an active twist rotor[J].IFAC Proceedings Volumes, 2010, 43(15):452-457
[22]BRILLANTE C, MORANDINI M, MANTEGAZZA P.Periodic controllers for vibration reduction using actively twisted blades[J].The Aeronautical Journal, 2016, 120(1233):1763-1784
[23]MITURA A, GAWRYLUK J.Experimental and finite element analysis of PPF controller effectiveness in composite beam vibration suppression[J].Eksploatacja i Niezawodno, 2022, 24(3):468-477
[24]GUO Y, YU Y, LI L, et al.Modeling and vibration control of a rotating flexible plate actuated by MFC[J].Composite Structures, 2024, 331:117907-
[25]KIM D H, HONG S, JUNG S N.Multicyclic Vibration Control of a Helicopter Rotor with Active Twist Actuation[J].International Journal of Aeronautical and Space Sciences, 2022, 23(2):303-314
[26]FOGARTY D E, WILBUR M, SEKULA M.A computational study of BVI noise reduction using active twist control[C]//American Helicopter Society 66th Annual Forum and Technology Display. Phoenix: American Helicopter Society, 2010, 1: 660-668.
[27]FOGARTY D E, WILBUR M, SEKULA M.The effect of non-harmonic active twist actuation on BVI noise[C]//AHS International 67th Annual Forum and Technology Display, 2011, 1: 37-46.
[28]ANOBILE A, BERNARDINI G, GENNARETTI M.Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation[C]//19th AIAA/CEAS Aeroacoustics Conference: American Institute of Aeronautics and Astronautics, 2013: 2290.
[29]ANOBILE A, BERNARDINI G, GENNARETTI M.Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation[J].International Journal of Acoustics and Vibration, 2016, 21(3):239-248
[30]ANOBILE A, BERNARDINI G, TESTA C, et al.Synthesis of a Rotor BVI Noise Active Controller Through an Efficient Aerodynamics/Aeroacoustics Solver[C]//20th AIAA/CEAS Aeroacoustics Conference, 2014: 3186.
[31]KEATS W W, L.W M, H. M P, et al. Aeroelastic Analysis of the NASA/ARMY/MIT Active Twist Rotor[C]//American Helicopter Society 55th Annual Forum. Montreal, Canada: American Helicopter Society, 1999.
[32]CESNIK C E S, SHIN S J, WILKIE W K, et al.Modeling, design, and testing of the NASA/Army/MIT active twist rotor prototype blade[C]//Proceedings of the American Helicopter Society 55th Annual Forum, Montreal, Canada, 1999.
[33]WILBUR M L, YEAGER W T, WILKIE W K, et al.Hover testing of the NASA/ARMY/MIT active twist rotor prototype blade[C]//56th American Helicopter Society Annual Forum. Virginia Beach, VA, US: American Helicopter Society, 2000.
[34]WILBUR M L, MIRICK P H, YEAGER W T, et al.Vibratory Loads Reduction Testing of the NASAArmyMIT Active Twist Rotor[J].Journal of the American Helicopter Society, 2002, 47(2):123-133
[35]WILBUR M L, YEAGER W T, SEKULA M K.Further examination of the vibratory loads reduction results from the NASA/Army/MIT active twist rotor test[C]//58th American Helicopter Society Annual Forum, 2002.
[36]SHIN S, CESNIK C E S, HALL S R.Closed Loop Control Test of the NASAArmyMIT Active Twist Rotor for Vibration Reduction[J].Journal of the American Helicopter Society, 2005, 50(2):178-194
[37]BERNHARD A P F, WONG J.Wind Tunnel Evaluation of a Sikorsky Active Rotor Controller Implemented on the NASAARMYMIT Active Twist Rotor[J].Journal of the American Helicopter Society, 2005, 50(1):65-81
[38]YEAGER W, WILBUR M, NIXON M.Review of Recent Rotorcraft Experimental Investigations in the Langley Transonic Dynamics Tunnel[C]//44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2003: 1963.
[39]SHIN S, CESNIK C E S, HALL S R.System Identification Technique for Active Helicopter Rotors[J].Journal of Intelligent Material Systems and Structures, 2005, 16(11-12):1025-1038
[40]SHIN S, CESNIK C, HALL S.Control of integral twist-actuated helicopter blades for vibration reduction[C]//AHS International, 58th Annual Forum Proceedings, 2002: 2122-2133.
[41]SHIN S, CESNIK C.Helicopter Performance and Vibration Enhancement by Twist-Actuated Blades[C]//44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2003: 1818.
[42]SHAW J, ALBION N.Active Control of the Helicopter Rotor for Vibration Reduction[J].Journal of the American Helicopter Society, 1981, 26(3):32-39
[43]陈钰, 宗群, 张秀云.直升机旋翼振动主动控制方法研究进展[J].哈尔滨工业大学学报, 2023, 55(8):1-17
[44]SHAW J.Higher harmonic blade pitch control: a system for helicopter vibration reduction[D]. Massachusetts Institute of Technology, 1980.
[45]RUBINACCI R, MERAGLIA S, LOVERA M.Continuous time adaptive Higher Harmonic Control[C]//Proceedings of the 2022 CEAS EuroGNC conference, 2022: 1-10.
[46]PRECHTL E F.Design and implementation of a piezoelectric servo-flap actuation system for helicopter rotor individual blade control[D]. Massachusetts Institute of Technology, 2000: 177-186.
[47]BOOTH E R, Wilbur M L.Acoustic Aspects of Active Twist Rotor Control[J].Journal of the American Helicopter Society, 2004, 49(1):3-10
[48]JACKLIN S A.Comparison of five system identification algorithms for rotorcraft higher harmonic control[R]. NASA/TP-1998-207687, Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
[49]PATT D, LIU L, CHANDRASEKAR J, et al.Higher-Harmonic-Control Algorithm for Helicopter Vibration Reduction Revisited[J].Journal of Guidance, Control, and Dynamics, 2005, 28(5):918-930