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2024, 04, No.226 16-29
Research progress of wide-range adaptive morphing aircraft technology
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DOI: 10.16358/j.issn.1009-1300.20240075
Published:   2024-07-25
Publication Date:   2024-07-25
Online:   2024-07-25
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Abstract:

With the rapid development of advanced materials, manufacturing processes and other technologies, intelligent morphing aircrafts which can adapt to different flight environment and missions become a research hotspot in order to better balance performance of wide-range flight. For aircraft in different speed ranges such as low-speed, transonic speed and supersonic speed, the application of variant technologies in aircraft is summarized. Various kinds of bionic variant technologies such as bird imitation and insect imitation are introduced, and the configurations and advantages of several common wing/rudder variants such as folding wing, telescopic wing and variable swept back wing are sorted out and summarized. The research progress of the low-speed, high-speed and ultra-high-speed aircraft with morphing function and key technologies of wide-range adaptation are emphasized. In the future, morphing aircraft will be developed around full-speed flight, lightweight design, intelligent variant and other aspects.

References

[1]陈树生,贾苜梁,刘衍旭,等.变体飞行器变形方式及气动布局设计关键技术研究进展[J].航空学报,2024,45(6):1-47.

[2]罗剑桥,刘晓东,马文朝,等.组合仿生跨介质飞行器设计及流固耦合性能研究[J].无人系统技术,2022,5(3):28-39.

[3]谢赞,周灿灿,赵振涛,等.宽速域飞行器发展及研究现状综述[J].空天技术,2022(4):28-39+86.

[4]许云涛.智能变形飞行器发展及关键技术研究[J].战术导弹技术,2017(2):26-33.

[5] Yuan Y Y. Review and analysis of variable swept wing technology[J]. International Journal of Modern Research in Engineering and Technology,2019,4(6):9-11.

[6]武宇飞,龙腾,毛能峰.跨介质变体飞行器设计优化技术进展[J].战术导弹技术,2020(4):29-40.

[7] Li D C,Zhao S W,Da R A,et al. A review of modelling and analysis of morphing wings[J]. Progress in Aerospace Sciences,2018,100:46-62.

[8]张尧,张婉,别大卫,等.智能变体飞行器研究综述与发展趋势分析[J].飞航导弹,2021(6):14-23

[9]王春彦.变体飞行器研究现状与关键技术分析[J].德州学院学报,2021,37(2):31-34.

[10]白鹏,陈钱,徐国武,等.智能可变形飞行器关键技术发展现状及展望[J].空气动力学学报,2019(3):426-443.

[11] Clarke R. Allen M,Dibley R,et al. Flight test of the F/A-18 active aeroelastic wing airplane[C]. AIAA Atmospheric Flight Mechanics Conference and Exhibit. San Francisco,USA,August 15-18,2005.

[12] Cumming S B,Smith M S,Ali A N,et al. Aerodynamic flight test results for the adaptive compliant trailing edge[C]. AIAA Atmospheric Flight Mechanics Conference,Washington,USA,June 13-17,2016.

[13] Cheung K,Cellucci D,Copplestone G,et al. Development of mission adaptive digital composite aerostructure technologies(MADCAT)[C]. 17th AIAA Aviation Technology,Integration,and Operations Conference,Denver,USA,June 5-9,2017.

[14] Kuzmina S,Ishmuratov F,Zichenkov M,et al. Wind tunnel testing of adaptive wing structures[M]. Morphing Wing Technologies. Amsterdam:Elsevier,2018:713-755.

[15] Marouf A,Simiriotis N,T?J B,et al. Smart morphing and sensing for the wings of the future[M]. Cham:Springer International Publishing, Berlin, 2022:17-36.

[16]陈钱,白鹏,李锋.可变形飞行器机翼两种变后掠方式及其气动特性机理[J].空气动力学学报,2012,30(5):658-663.

[17]戎佳欣.自适应鼓包进气道结构的柔性蒙皮技术研究[D].南京:南京航空航天大学,2018.

[18]冉茂鹏,王成才,刘华华,等.变体飞行器控制技术发展现状与展望[J].航空学报,2022,43(10):424-441.

[19]贺媛媛,韩慧,王琦琛,等.微小型仿生扑翼飞行器研究进展及关键技术概述[J].战术导弹技术,2023(1):39-50.

[20] Abdulrahim M, Lind R. Control and simulation of a multi-role morphing micro air vehicle[R]. AIAA Journal,2005.

[21] Send W,Fischer M,Jebens K,et al. Artificial hingedwing bird with active torsion and partially linear kinematics[C]. Congress of the International Council of the Aeronautical Sciences, Brisbane, Australia, September23-28,2012.

[22] Mackenzie D. A flapping of wings[J]. Science,2012,335(6075):1430-1433.

[23] Jitsukawa T, Adachi H, Abe T, et al. Bio-inspired wing-folding mechanism of micro air vehicle(MAV)[J]. Artificial Life&Robotics,2017,22(2):1-6.

[24] Ramezani A,Chung S,Hutchinson S. A biomimetic robotic platform to study flight specializations of bats[J].Science Robotics,2017,2(3):2505.

[25] Khan Z,Steelman K,Agrawal S. Development of insect thorax based flapping mechanism[C]. 2009 IEEE International Conference on Robotics and Automation,Kobe,Japan,May 12-17,2009.

[26]王仲文,李振,段瑞珍.一种仿蜻蜓扑翼飞行器的设计与研究[J].哈尔滨理工大学学报,2020,25(6):98-106.

[27] Karásek M,Muijres F,Remes B,et al. A tailless aerial robotic flapper reveals that flies use torque coupling in rapid banked turns[J]. Science,2018,361(6407):1089-1094.

[28] Ajanic E, Feroskhan M, Mintchev S, et al. Bioinspired wing and tail morphing extends drone flight capabilities[J]. Science Robotics,2020,5(47):2897.

[29] Chang E,Matloff L Y,Stowers A K,et al. Soft biohybrid morphing wings with feathers underactuated by wrist and finger motion[J]. Science Robotics, 2020, 5(38):1246.

[30]梁友鉴,赵杰亮,阎绍泽.基于蜜蜂腹部变体机制的空天飞行器仿生变体头锥设计[J].机械工程学报,2020,56:47-54.

[31]甄子洋,刘攀,陆宇平.变体飞行器智能变形与飞行控制技术研究进展[J].南京航空航天大学学报,2022,54(6):995-1006.

[32]马航,宋笔锋,周忠彬,等.多段式变形翼技术发展现状分析[J].战术导弹技术,2024(1):75-84+112.

[33]李雪江,刘峰,乔宇.变体飞行器发展现状与应用前景[J].飞机设计,2022,42(5):1-7+13.

[34]肖洪,郭宏伟,张蒂,等.一种基于四面体单元的变形翼骨架设计与分析[J].航空学报,2022,43(7):410-419.

[35] Tian Y Z,Zhu Y,Zhao Y J,et al. Optimal design and analysis of a deformable mechanism for a redundantly driven variable swept wing[J]. Aerospace Science and Technology,2024,146:108993.

[36] Yang G,Guo H W,Liu R Q. Design and analysis of a variable-span and cambered span morphing wing for UAV[C]. 2019 IEEE International Conference on Robotics and Biomimetics(ROBIO), Dali, China, January 06-08,2019.

[37]冷劲松,孙健,刘彦菊.智能材料和结构在变体飞行器上的应用现状与前景展望[J].航空学报,2014,35(1):29-45.

[38]苏晓东.一种U型变体无人飞行器气动外形技术研究[J].中国科技信息,2020(5):38-41.

[39]宫晓博.基于变刚度蒙皮和零泊松比蜂窝的变弯度机翼结构研究[D].哈尔滨:哈尔滨工业大学,2017.

[40] Li Y,Ge W,Zhou J,et al. Design and experiment of concentrated flexibility-based variable camber morphing wing[J]. Chinese Journal of Aeronautics, 2022, 35(5):455-469.

[41]张欣,季宏丽,周丹杰,等.高超声速飞行器变体机翼方案及气动特性分析[J].航空工程进展,2023,14(4):47-57.

[42]陈小雨,杨睿,李扬,等.变体飞行器的折转翼尖设计及分析[J].现代机械,2021(4):59-63.

[43]彭悟宇,杨涛,涂建秋,等.高超声速变形飞行器翼面变形模式分析[J].国防科技大学学报,2018,40(3):15-21.

[44]焦子涵,付秋军,邓帆,等.全速域可变形飞行器气动布局设计及试验研究[J].固体火箭技术,2017,40(5):653-659.

[45]杨政,甄子洋,蒋烁莹,等.近空间可变翼飞行器小翼切换自适应控制方法[J].哈尔滨工程大学学报,2019,40(5):886-891.

[46]甄子洋,朱平,江驹,等.基于自适应控制的近空间高超声速飞行器研究进展[J].宇航学报,2018,29(4):335-367.

[47]杨博,朱一川,魏延明,等.折叠式变体飞行器轨迹优化及控制分析[J].中国空间科学技术,2020,40(3):64-75.

[48]梁尚军,杨珂,牛小康,等.变体飞机结构领域研究进展[J].飞机设计,2017,37(6):1-5.

[49] Bae J S, Seigler T M, Inman D, et al. Aerodynamic and aeroelastic considerations of a variable-span morphing wing[C]. AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics&Materials Conference, Palm Springs,USA,April 19-22,2004.

[50] Bae J S,Seigler T M,Inman D. Aerodynamic and static aeroelastic characteristics of a variable-span morphing wing[J]. Journal of Aircraft, 2005, 42(2):528-534.

[51]陈铁彪,王洪波,康永来,等.变形技术在助推-滑翔飞行器中的应用前景分析[J].战术导弹技术,2017(5):1-5+11.

[52]陈克,金玲,雷豹,等.高速飞行器折叠翼/舵设计技术与进展研究[J].强度与环境,2022(1):53-59.

[53]魏东辉,陈万春,李娜英,等.智能变形导弹变形机理及协调控制机制研究[J].战术导弹技术,2016(2):10-15.

[54] Yi L, Li Y, Ma L Z, et al. Analysis of aerodynamic characteristics of missile with different sweep angle under supersonic condition[J]. Journal of Physics:Conference Series,2021,1802(4):042003.

[55]韩光松,李萍.巡航导弹智能变形研究[J].舰船电子工程,2019,39(10):62-66.

[56]贾昂,王旭刚,李广.变体制导炮弹气动特性分析及弹道仿真[J].弹道学报,2022,34(4):74-82.

[57]高良.弹射式变掠角串置翼飞行机器人设计及控制方法研究[D].哈尔滨:哈尔滨工业大学,2020.

[58]王俊伟,冯丽,叶蕾,等. 2022年国外高超声速领域发展研究[J].战术导弹技术,2023(2):15-24.

[59]张登成,罗浩,张艳华,等.宽速域变构型高超声速飞行器气动特性研究[J].固体火箭技术,2019(1):128-134.

[60] Liu B,Liang H,Han Z H,et al. Surrogate-based aerodynamic shape optimization of a morphing wing considering a wide Mach-number range[J]. Aerospace Science&Technology,2022,124:107557.

[61]陆宇平,刘张.可变形乘波体气动推进与控制一体化综合设计[J].南京航空航天大学学报,2011,43(2):252-256.

[62]黄明晗.高超声速变形飞行器设计与弹道优化[D].长沙:国防科学技术大学,2023.

[63]戴今钊,汤继斌,陈海昕.高超声速飞行器中的乘波设计综述[J].战术导弹技术,2021(4):1-15.

[64] Bowcutt K G. Hypersonic waverider variable leading edge flaps:US,2003205640[P]. 2003-10-21.

[65] Takama Y. Practical waverider with outer wings for the improvement of low-speed aerodynamic performance[C]. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference,San Francisco,CA(US),April 11-14,2011.

[66]刘晓斌.高超声速飞行器变构型方式探索研究[J].战术导弹技术,2018(4):1-5.

[67]吴世超.全速域乘波飞行器变体气动布局设计技术研究[D].长沙:国防科技大学,2018.

[68]罗浩,张登成,张艳华,等.宽速域高超声速飞行器设计与气动特性研究[J].飞行力学,2019,37(2):26-30.

[69] Dai P,Yan B B,Huang W,et al. Design and aerodynamic performance analysis of a variable sweep-wing morphing waverider[J]. Aerospace Science and Technology,2020,98:105703.

[70]朱睿颖,齐征,王兰松,等.可变构型飞行器航迹优化设计[J].战术导弹技术,2020(5):157-164.

[71]闫韬.高超声速变体飞行器变体机构设计与仿真分析[D].北京:北京信息科技大学,2022.

[72] Maxwell J R. Hypersonic waverider stream surface actuation for variable design point operation[C]. 52nd AIAA/SAE/ASEE Joint Propulsion Conference,Salt Lake City,USA,July 25-27,2016.

[73] Liu Z, Liu J, Ding F, et al. Novel methodology for wide-ranged multistage morphing waverider based on conical theory[J]. Acta Astronautica, 2017, 140:362-369.

[74] Phoenix A A,Maxwell J R. The mach 5 to 3. 5 morphing waverider optimal actuation location selection[C]. 2018AIAA/AHS Adaptive Structures Conference, Kissimmee,USA,January 8-12,2018.

[75] Phoenix A A,Rogers R E,Maxwell J R,et al. Mach five to ten morphing waverider:Control point study[J].Journal of Aircraft,2019,56(2):493-504.

[76] Sun J, Du L Z, Scarpa F, et al. Morphing wingtip structure based on active inflatable honeycomb and shape memory polymer composite skin:A conceptual work[J]. Aerospace Science&Technology, 2021,111:106541.

[77] Azzawi W A. Development and performance evaluation of a morphing wing design using shape memory polymer and composite corrugated structure[J]. Australian Journal of Mechanical Engineering,2022,22(1):12-26.

[78] Kim N G,Han M W,Iakovleva A,et al. Hybrid composite actuator with shape retention capability for morphing flap of unmanned aerial vehicle(UAV)[J]. Composite Structures,2020,243:112227.

[79] Hao L,Qiu J H,Ji H L,et al. Numerical analysis on shape memory alloy-based adaptive shock control bump[J]. Journal of Intelligent Material Systems and Structures,2018,29(15):3055-3066.

[80] Gu X J,Yang K K,Wu M Q,et al. Integrated optimization design of smart morphing wing for accurate shape control[J]. Chinese Journal of Aeronautics,2021,34(1):135-147.

[81]尹维龙,石庆华.变体飞行器蒙皮材料与结构研究综述[J].航空制造技术,2017,(17):24-29.

[82]杨森,刘峰,聂瑞,等.变体飞行器智能材料驱动器和柔性蒙皮研究进展[J].航空工程进展,2024,15(3):1-12+26.

[83] Radestock M, Riemenschneider J, Falken A, et al.Experimental study of flexible skin designs between a moving wing segment and a fixed wing part on a full scale demonstrator[C]. ASME 2020 Conference on Smart Materials, Adaptive Structures and Intelligent Systems,Virtual,Online,September 15,2020.

[84]冯宁.基于气动肌肉纤维的主动变形蒙皮结构性能研究[D].哈尔滨:哈尔滨工业大学,2016.

[85] Wu R,Sun J,Chang Z Z,et al. Elastic composite skin for a pure shear morphing wing structures[J]. Journal of Intelligent Material Systems and Structures, 2015, 26(3):352-363.

[86] Yu J R,Ma J Y. Design and shear analysis of an angled morphing wing skin module[J]. Applied Sciences,2022,12(3092):3092.

[87] Rafsanjani A,Akbarzadeh A,Pasini D. Snapping mechanical metamaterials under tension[J]. Advanced Materials,2015,27(39):5931-5935.

[88] Zadeh M N,Dayyani I,Yasaee M. Fish Cells,a new zero Poisson's ratio metamaterial—Part I:Design and experiment[J]. Journal of Intelligent Material Systems and Structures,2020,31(13):1617-1637.

[89] Jha A,Dayyani I. Shape optimisation and buckling analysis of large strain zero Poisson's ratio Fish-cells metamaterial for morphing structures[J]. Composite Structures,2021,268:113995.

[90] Han Z T, Wang Z G, Wei K. Shape morphing structures inspired by multi-material topology optimized bifunctional metamaterials[J]. Composite Structures,2022,300:116135.

[91] Matthew B D,Phillips F R,Henry T C,et al. Spanwise wing morphing using multistable cellular metastructures[J]. Extreme Mechanics Letters, 2022, 53:101706.

[92]王鹏飞,蒋坤,张峰.高超声速飞行器输入受限反步控制[J].战术导弹技术,2023(2):57-65.

[93]汪雨劼,杜翔宇,刘磊,等.基于鲁棒自适应动态规划的临近空间飞行器姿态跟踪控制[J].战术导弹技术,2022(2):75-82.

[94]万航,徐胜利,张庆振,等.基于动态逆的空天变体飞行器姿态控制[J].空天防御,2019, 2(4):25-31.

[95] Ouyang Y,Gu Y S,Kou X P,et al. Active flutter suppression of wing with morphing flap[J]. Aerospace Science&Technology,2021,110:106457.

[96]曹承钰,廖宇新,曹玉腾,等.基于气动参数辨识的变体飞行器自适应控制方法[J].控制与信息技术,2022(3):8-16.

[97]张泽鹏,院老虎,杜白雨,等.变体飞行器LPV建模与内外环鲁棒控制[J].战术导弹技术,2023(1):105-114.

[98]梁帅,杨林,杨朝旭,等.基于Kalman滤波的变体飞行器T-S模糊控制[J].航空学报,2020(S02):58-65.

[99]闫斌斌,李勇,戴沛,等.基于增强学习的变体飞行器自适应变体策略与飞行控制方法研究[J].西北工业大学学报,2019,37(4):656-663.

[100] Qiao F X,Shi J P,Qu X B,et al. Adaptive backstepping neural control for an embedded and tiltable Vtail morphing aircraft[J]. International Journal of Control, Automation and Systems, 2022, 20(2):678-690.

[101] Wang E M,Lu H,Zhang J C,et al. A novel adaptive coordinated tracking control scheme for a morphing aircraft with telescopic wings[J]. Chinese Journal of Aeronautics,2024,37(2):148-162.

[102] Gong L G,Wang Q,Hu C H,et al. Switching control of morphing aircraft based on Q-learning[J]. Chinese Journal of Aeronautics,2020,33(2):672-687.

[103] Hou L,Liu H,Yang T,et al. An intelligent autonomous morphing decision approach for hypersonic boostglide vehicles based on DNNs[J]. Aerospace, 2023,10(12):1008.

[104]储培,倪昆,程林,等.基于反步滑模的高超声速变体飞行器鲁棒控制[J].计算机仿真,2018,35(8):41-45.

[105]杨芊,胡来红,张艳红,等.基于不确定LPV系统的变体飞行器姿态控制[J].兵器装备工程学报,2023,44(10):127-133.

[106] Bao C Y, Wang P, Tang G J. Integrated method of guidance,control and morphing for hypersonic morphing vehicle in glide phase[J]. Chinese Journal of Aeronautics,2021,34(5):535-553.

Basic Information:

DOI:10.16358/j.issn.1009-1300.20240075

China Classification Code:V27;V47

Citation Information:

[1]Ke Zhiqian,Luo Junheng,Ma Rui ,et al.Research progress of wide-range adaptive morphing aircraft technology[J].Tactical Missile Technology,2024,No.226(04):16-29.DOI:10.16358/j.issn.1009-1300.20240075.

Fund Information:

国家自然科学基金(12372272)

Published:  

2024-07-25

Publication Date:  

2024-07-25

Online:  

2024-07-25

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