[1] 邓景辉.直升机技术发展与展望[J].航空科学技术,2021,32(1):10-16.
DENG J H.Development and prospect of helicopter technology[J].Aeronautical Science and Technolo-gy,2021,32(1):10-16(in Chinese).
[2] BENTLEY C E,SISSON M L. Joint future vertical Lift (FVL) Initiative[C]// The AHS International 71th Annual Forum & Technology Display. Virginia Beach: AHS, 2015:1-10.
[3] EHING R,MC M,WILSON P. Bell V-280 Valor: JMR TD Flight Test Update-Year2[C]// The Vertical Flight So-ciety’s 75th Annual Forum & Technology Display. Phila-delphia: AHS, 2019:1-8.
[4] BOWLES P O,MATALANIS C,BATTISTI M,et al. Full-Configuration CFD Analysis of the S-97 RAIDERTM[C]// The VFS 75th Annual Forum & Tech-nology Display, Philadelphia: AHS, 2019:1-12.
[5] LORBER P,BOWLES P,FOX E. Wind tunnel testing for the SB>1 defiant joint multi-role technology demonstra-tor[C]//The AHS International 73rd Annual Forum & Technology Display, Texas, 2017:1-18.
[6] EHINGER R,MC M,WILSON P. Bell V-280 valor: a flight test update[C]// The AHS International 74th Annual Forum & Technology Display. Phoenix: AHS, 2018:1-13.
[7] Defense Science Board Washington DC. Technology and Innovation Enablers for Superiority in 2030: ADA608507[R].Washington DC:Defense Science Board, 2013.
[8] BLACHA M,FINK A,EGLIN P,et al. ."Clean Sky 2"：exploring new rotorcraft high speed configura-tions[C]//The 43rd European Rotorcraft Foru. Mi-lan:ERF,2017:1-12.
[9] BLACHA M,GARCIA R A,SCHELCHER M. The challenges for the integration of the drive shaft in the rac-er's wing configuration [C]// The Vertical Flight Society 75th Annual Forum & Technology Display. Pennsylvania: AHS, 2019:1-11.
[10] GARCIAA A,BARAKOS G N. Numerical simulations on the ERICA tiltrotor[J].Aerospace Science and Tech-nology, 2017:171-191.
[11] MAISEL M D,GIULIANETTI D J,DUGAN D C. The history of the xv-15 tilt rotor research aircraft : NASA SP-2000-4517[R].Washington: NASA, 2000.
[12] DETORE J A,GAFFEY T M.The stopped-rotor variant of the proprotor VTOL aircraft[J]. Journal of the Ameri-can Helicopter Society,1970,15(3):45-56.
[13] CHERY M C, SUPERVISOR J. The ABC helicop-ter[C]// AIAA/AHS VTOL Research, Design, and Oper-ations Meeting. Atlanta:AIAA, 1969:1-5.
[14] ROSENSTEIN H. Aerodynamic development of the V-22 tilt rotor[C]// The 12th European Rotorcraft Forum, Garmisch: ERF, 1986:1-30.
[15] WENTRUP M,YIN J,KUNZE P, et al. An overview of DLR compound rotorcraft aerodynamics and aeroa-coustics activities within the cleansky2 NACOR pro-ject[C]//The AHS International 74th Annual Forum & Technology Display. Phoenix: AHS, 2018: 1-16.
[16] SCHRAGE D P, STANZIONE K. Assessing the impact of hybrid distributed electric propulsion on VTOL air-craft design & system effectiveness[C]//The AHS Inter-national 74th Annual Forum &Technology Display. Phoenix: AHS, 2018:1-11.
[17] RUDDELL A J. Advancing blade concept (ABC) tech-nology demonstrator: TR-81-d-5[R]. Stratford: AVRADCOM, 1981.
[18] ARTHUR W L, SIMON D.XH-59A ABCTM aircraft flight tests at ft. rucker alabam[J].Aircraft Engineer-ing ,1982:1-5.
[19] BAGAI A. Aerodynamic design of the x2 technology demonstrator main rotor blade[C]//The 64th Annual Na-tional Forum of AHS. Montreal: AHS, 2008: 1-16.
[20] ARENTS D N. An assessment of the hover performance of the xh-59a advancing blade concept demonstration helicopter:USAAMRDL-TN-25[R]. Fort:USAAMRDL,1977.
[21] WALSH D,WEINER S, ARIFIAN K, et al. Develop-ment testing of the sikorsky x2 technology? demonstra-tor[C]// The 65th Annual Forum of the American Heli-copter Society International. Grapevine: AHS, 2009:1-11.
[22] BOUWER S, KAISER E. Design and development of the main rotor gearbox for the sikorsky boeing sb>1 de-fiant jmr technology demonstrator aircraft[C]// The Verti-cal Flight Society’s 75th Annual Forum &Technology Display. Philadelphia: AHS, 2019:1-9.
[23] PATRYHOW R. Sikorsky adapted to meet the u.s. army fara program timeline[C]// The Vertical Flight Society’s 77th Annual Forum & Technology Display. Virtual: AHS,2021:1-11.
[24] 徐敏.倾转旋翼机的发展与关键技术综述[J].直升机技术,2003,(2):40-44.
XU M.The development and key technology review of the tilt-rotor aircraft[J]. Helicopter Technique,2003,(2): 40-44(in Chinese).
[25] 陈恒,左晓阳,张玉琢等.倾转旋翼飞机技术发展研究[J].飞行力学,2007,25(1):5-8(in Chinese).
CHEN H,ZUO X Y,ZHANG Y Z,et al. Research on the development of tilt-rotor aircraft technology[J]. Flight Dynamics,2007,25(1)：5-8.
[26] THOMASON T H.The bell helicopter XV-3&XV-15 experimental aircraft-lessons learned[J].AIAA-90-3265-CP:1-10.
[27] MEHRA R K,PRASANTH R K,GOPALAWAMY S. XV-15 tilt-rotor flight control system design using model predictive control[C]//Aerospace Conference, IEEE,1998.
[28] 薛蒙,孙强.倾转旋翼机军事需求与关键技术分析[J].直升机技术,2020,(1):47-49,27.
XUE M,SUN Q. The military demand and key technical analysis of the tilt-rotor aircraft[J]. Helicopter Technique, 2020,(1):47-49,27(in Chinese).
[29] 杨军，吴希明，凡永华等.倾转旋翼机飞行控制[M].航空工业出版社，2006.
YANG J,WU X M,FAN Y H,et al. Flight control of the tilt-rotor aircraft[M]. Aviation industry press,2006(in Chinese).
[30] 张庆,殷永亮,吴超等.美军倾转旋翼机的发展和事故分析[J].科学之友,2011,(15):126-128.
ZHANG Q,YIN Y L,WU C.Development and Crash Analysis of The American Army Inclines and Transfers to the Gyroplane[J].Friend of Science Ama-teurs,2011,(15):126-128(in Chinese).
[31] BOLKCOM C.V-22 osprey tilt-rotor air-craft[J].Congressional Research Service Reports,2005.
[32] GERYLER J. V-22 Osprey tilt-eotor aircraft：background and issues for congress, congressional re-search service[J],CRS Report for Congress,2011.
[33] 肖江涛.新型无人倾转旋翼机过渡状态飞行控制律设计[D].南京航空航天大学,2021.
XIAO J T.Design of Flight Control Law for New Con-figuration Unmanned Tilt-rotor Aircrafit in Transiton Atate[D].NUAA,2021(in Chinese).
[34] 刘乾坤.电驱无人倾转旋翼飞行器动力总成设计与仿真[D].南京航空航天大学,2020.
LIU Q K, Design and Simulation of Electric Drive Un-manned Tilting Rotorcraft Powertrain[D].NUAA, 2020(in Chinese).
[35] 尹欣繁,车兵辉,章贵川等.国外复合式高速直升机发展现状与关键技术[J].飞航导弹,2019,(11):56-60.
YIN X F,CHE B H,ZHANG G C,et al. The status and key technologies of multi-type high-speed helicopter de-velopment in foreign countries[J].Aerodynamic Missile Journal,2019,(11):56-60(in Chinese).
[36] 余震,王永红.复合式高速直升机传动系统关键技术分析[J].航空动力学报,2018,(3):66-68.
YU Z,WANG Y H. Key technical analysis of compound high-speed helicopter transmission system[J]. Journal of Aerospace Power, 2018,(3):66-68(in Chinese).
[37] 黄明其,徐栋霞,何龙等.常规旋翼构型复合式高速直升机发展概况及关键技术[J].航空动力学报,2021,36(6):1156-1168.
HUANG M Q,XU D X,HE L,et al. The development of conventional rotor configuration compound high-speed helicopter development and key technology[J]. Journal of Aerospace Power,2021,36(6):1156-1168(in Chinese).
[38] 丁达文.单旋翼复合式高速直升机动力学建模及振动特征分析[D].南京航空航天大学,2021.
DING D W. Modeling and vibration characteristics of single-rotor complex high-speed helicopter[D]. Journal of Nanjing University of Aeronautics & Astro-nautics,2021(in Chinese).
[39] 何振亚.复合式高速直升机飞行性能研究[D].南京航空航天大学,2021.
HE Z D. Research on the performance of compound high-speed helicopter flight[D]. Journal of Nanjing Uni-versity of Aeronautics & Astronautics,2021(in Chinese).
[40] HEAD E. Vahana eVTOL aims for“direct to autono-my”[M],2018.
[41] David D.North, Ronald C.Busan, Greg Howland. De-sign and Fabrication of the Langley Aerodrome[C]// 8th Distributed Electric Propution VTOL Tested. AIAA Scitech Forum, 2021.
[42] AIRBUS. Vahana has come to an end. But a new chapter at Airbus has just begun[M].2019.
[43] DAVID D N, RONALD C B, GREG H. Design and fabrica-tion of the langley aerodrome no.8 distributed electric pro-pution VTOL tested[M].2021.
[44] ROBERT W M. NASA’s LA-8: generating public eV-TOL data[M].2022.
[45] Bagai A. Aerodynamic Design of the X2 Technology De-monstrator Main Rotor Blade[C]//The 64th Annual Na-tional Forum of AHS, Montreal, 2008: 1-16.
[46] Peter F,Zhao J G, et al. S-97 RAIDER wake-empennage interaction flight data and correlation [C]//The 77th An-nual Forum of the VFS, Fairfax, 2021.
[47] George Jacoellis, Farhan Gandhi. Investigation of per-formance loads and vibrations of a coaxial helicopter in high speed-flight [C]//The 72nd Annual Forum of the AHS, West Palm Beach,2016.
[48] SYAL M,LEISHMAN J G. Aerodynamic optimization study of a coaxial eotor in hovering flight[J]. Journal of the American Helicopter Society, 2012,57(4):1-15.
[49] LEISHMAN J G ,SYAL M. Figure of merit definition for coaxial rotors[J]. Journal of the American Helicopter Society, 2008,53(3):290.
[50] Tom Berger, Chris L. Flight control design and simula-tion handling qualities assessment of high-speed ro-torcraft [C]//The 75th Annual Forum of the VFS, Phila-delphia, 2019.
[51] Umberto Saetti. Rotorcraft flight control design with alleviation of unsteady rotor loads [D]. Pennsylvania State University, USA, 2019.
[52] Walsh D, Weiner S, et al. High airspeed testing of the Sikorsky X2 Technology(TM) demonstrator [C]//The 67th Annual Forum of the AHS, Virginia Beach, 2011.
[53] Erez Eller.X2? Load Alleviating Controls [C] //The 68th Annual Forum of AHS, Texas, 2012: 1-3.
[54] Blackwell R. and Millot T. Dynamics design characteris-tics of the Sikorsky X2 technology demonstrator air-craft[C]//The 64th AHS Annual Forum Proceedings, Montreal, 2008: 1-13
[55] Hyeonsoo Yeo, Wayne Johnson. Investigation of Maxi-mum Blade Loading Capability of Lift-Offset Ro-tors[C]//Presented at the AHS 69th Annual Forum, Phoenix, Arizona,2013: 21–23.
[56] Jeong In go, Do Hyung kim, Jae Sang park. Perfor-mance and Vibration Analyses of Lift-Offset Helicop-ters[J]. Ineternational Journal of Aerospace Engineering, 2017.
[57] Joseph Schmaus, Inderjit Chopra. Performance and Loads of a Model Coaxial Rotor Part II Prediction Vali-dations[C]//The 72th Annual Forum of the AHS, West Palm Beach, Florida, 2016.
[58] LEE Y L,KIM D H,PARKA J S. Vibration reduction simulations of alift-offset compound helicopter using two active control techniques[J]. Aerospace Science and Technology,2020:106-181.
[59] KWON Y M,HONG S B,PARK J S,et al. Active vibra-tion reductions of a lift-offset compound helicopter using individual blade pitch control with multiple harmonic in-puts[J]. Aircraft Engineering and Aerospace Technology. 2022,94/6 :994–1008.
[60] BANG S W,HONG S B，BEEN Y,et al. Active airframe vibration control study using a small-scale model for lift-offset compound helicopter[J]. International Journal of Aeronautical and Space Sciences, 2023,24:77-91.
[61] R. Blackwell, T. Millott.Dynamics Design Characteristics of the Sikorsky X2 TechnologyTM Demonstrator Air-craft[C]//The 64th Annual Forum of the AHS, West Palm Beach, Florida, 2008.
[62] Rysdyk R, Calise A J, Chen R T N. Nonlinear adaptive control of tiltrotor aircraft using neural networks[R]. SAE Technical Paper, 1997.
[63] 刘佳豪,李高华,王福新.倾转过渡状态旋翼-机翼气动干扰特性计算分析[J]. 航空学报,2022, 43(7):1-10.
LIU J H, LI G H,WANG F X. Calculation Analysis of Rotor-Wing Aerodynamic Interference Characteristics in Conversion Mode[J]. Acta Aeronautica et Astronautica Sinica, 2022,43(7):1-10(in Chinese).
[64] Rysdyk R, Calise A J, Chen R T N. Nonlinear adaptive control of tiltrotor aircraft using neural networks[R]. SAE Technical Paper, 1997.
[65] Sobol I M, Statnikov R B. Selecting optimal parameters in multicriteria problems [C]//The 2nd ed. Moscow: Dro-fa, 2006: 89-105.
[66] Bell V-280 system identification and model validation with flight test data using the joint input-output meth-od[C]//Ertical Flight Society’s 76th Annual Forum & Technology Display, Virtual ,2020:6-89.
[67] 董凌华.倾转旋翼回转颤振参数影响规律研究[J].航空科学技术,2015,15(11):49-55.
Dong L H. Research on the influence rules of Proprotor flutter parameters of tilting rotor[J]. Aeronautical Science & Technology, 2015,15(11):49-55(in Chinese).
[68] Acree C W,Peyran R J,Johnson W.Rotor Design Options for Improving Tiltrotor Whirl-Flutter Stability Mar-gins[J].Journal of the American Helicopter Society, 2001, 46(2):87-95.
[69] Vanaken J M. Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active con-trols[C]//The 47th AHS Annual Fo-rum,Phoenix,AZ,Proceedings,1991,26:1-27.
[70] 王福新,黄明其.倾转旋翼飞行器的风洞试验技术综述[J].试验流体力学,2005,19(4):86-89.
WANG F X,HUANG M Q.A summary on the wind tunnel test techniques for tilting rotor aircraft[J].Journal of Experiments in Fluid Mechanics,2005,19(4):86-89(in Chinese).
[71] Yeo H. Investigation of UH-60A Rotor Performance and Loads at High Advance Ratios[C]//The American Heli-copter Society 68th Annual Forum., Texas: AHS, 2012:576-587.
[72] Frey F, Thiemeier J, Ohrle C, et al. Aerodynamic Interac-tions on Airbus Helicopters' Compound Helicopter RACER in Cruise Flight[C]//The Vertical Flight Society 75th Annual Forum & Technology Display. Pennsylvania: AHS, 2019:1-19.
[73] TOROPOV M Y,STEPANOV S Y. Modeling of heli-copter flight imitation in the vortex ring state[J].Russian Aero-nautics(Iz VUZ),2016,59(4):517-522.
[74] ORCHARD M, SOUYHAMPTON U O, NAW-MANS, et al. Some design issues for the optimization of the compound helicopter configuration[C]//Proceedings of American Heli-copter Society 56th Annual Forum. Virginia Beach, Virginia: AHS, 2000.
[75] THORSEN A T. A unified control methodology for a compound rotorcraft in fundamental and aerobatic ma-neuvering flight[EB/OL]. 2016. https://etda.libraries.psu.edu/files/final_submissions/13553.
[76] Ronan B. Numerical analysis of rotor/propeller aerody-namic interactions on high speed compound helicopter[J]. Journal of the American Helicopter Society, 2022, 67(1), 1-15.
[77] Constantin O, Felix F, Jakob T, et al. Compound helicop-ter X3 in high speed flight: correlation of simulation and flight test[C]//The Vertical Flight Society 75th Annual Forum and Technology Display, Philadelphia, 2019:836-874.
[78] Hoover CB, Shen J, Kreshock Ar. Propeller Whirl Flut-ter Stability And Its Influence On X-57 Aircraft De-sign[J]. Jour-nal of Aircraft, 2018, 55(5): 2169-2175.
[79] RONALD C B, PATRICK C M, DAVID B H, BENJAMIN M S. Wind tunnel testing techniques for a tandem tilt-wing distributed electric propulsion VTOL aircraft[M].2020.
[80] KATHY B. Ten-engine electric plane completes success-ful flight test [EB/OL].[2015-11-24].
[81] GRAHAM WARWICK,徐德康. NASA 的多发 VTOL 无人机进行飞行试验[J].国际航空,2015(6):76-77.
GRAHAM WARWICK,XU D K.NASA Multiple VTOL Drones Fly Tests[J].International Avia-tion,2015(6):76-77(in Chinese).
[82] Hoover CB, Shen J, Kreshock Ar. Propeller Whirl Flut-ter Stability And Its Influence On X-57 Aircraft De-sign[J]. Jour-nal of Aircraft, 2018, 55(5): 2169-2175.
[83] Mills B, Datta A. Fundamental Studies Of Variable-Voltage Hybrid-Electric Powertrains[J]. Journal of the American Helicopter Society, 2021, 66(2): 1-14.
[84] 王伟,周洲,祝小平等.基于 CR 理论的大柔性太阳能无人机非线性配平及飞行载荷分析[J].西北工业大学学报,2015,(4):566-572.
WANG W,ZHOU Z,ZHU X P. CR Approach of Nonlin-ear Trim and Flight Load Analysis of Very Flexible Solar Powered UAV[J].Journal of Northwestern Polytech-nicalUniversi-ty,2015,(4):566-572(in Chinese).
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