飞机阵风响应减缓技术综述

doi:10.7527/S1000-6893.2021.27350

Abstract

Abstract: To reduce the impact of gust on aircraft flight performance and safety, the structure of the aircraft was often strengthened to resist gusts interference in the early days. Since the 1950s, the gust alleviation technology based on active control has been gradually developed and successfully applied to many practical aircrafts, effectively reducing the gust response and improving the fatigue life and flight quality of aircraft. Domestic related research started late, and the engineering application of gust alleviation has been put on the agenda due to the demand of domestic large aircraft projects. This paper puts forward the general technical route of aircraft gust alleviation, and summarizes the historical development and research status of the following technologies according to this route. Firstly, the basic mathematical models of gust alleviation are introduced, involving the aircraft dynamics model, gust model, unsteady aerodynamic model and gust response analysis method. Secondly, the design methods of gust alleviation are analyzed in terms of alleviation mechanism and control law design. The specific cases of gust alleviation wind tunnel test and flight test and practical applications are reviewed. Finally, the frontier progress of gust alleviation research is summarized and the key technical problems that need to be solved urgently are discussed, providing insights for scientific research and engineering technicians in this field.

Key words: gust response, gust alleviation, aeroelasticity, active control, wind tunnel test, flight test

CLC Number:

V217⁺.39

YANG Chao, QIU Qisheng, ZHOU Yitao, WU Zhigang. Review of aircraft gust alleviation technology[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527350.

References

[1] HUNSAKER J C, WILSON E B. Report on behavior of aeroplanes in gusts:NACA-TR-1[R]. Washington, D.C.:NASA, 1917.
[2] HOUBOLT J C. Atmospheric turbulence[J]. AIAA Journal, 1973, 11(4):421-437.
[3] 沈强, 沈文武. 一种新的预报晴空湍流综合算法[J]. 气象与减灾研究, 2009, 32(2):44-49. SHEN Q, SHEN W W. A new synthesis algorithm for clear air turbulence forecast[J]. Meteorology and Disaster Reduction Research, 2009, 32(2):44-49(in Chinese).
[4] DISNEY T E. C-5A active load alleviation system[J]. Journal of Spacecraft and Rockets, 1977, 14(2):81-86.
[5] JOHNSTON J F. Accelerated development and flight evaluation of active controls concepts for subsonic transport aircraft. Volume 1:Load alleviation/extended span development and flight tests:NASA-CR-159097[R]. Washington, D.C.:NASA, 1979.
[6] WYKES J, BORLAND C, KLEPL M, et al. Design and development of a structural mode control system:NASA/CR-1977-143846[R]. Washington, D.C.:NASA, 1977.
[7] BRITT R, VOLK J, DREIM D, et al. Aeroservoelastic characteristics of the B-2 bomber and implications for future large aircraft:ADP010486[R]. Virginia:Defense Technical Information Center, 1999.
[8] REGAN C, JUTTE C. Survey of applications of active control technology for gust alleviation and new challenges for lighter-weight aircraft:NASA/TM-2012-216008[R]. Washington, D.C.:NASA, 2012.
[9] HOBLIT F M. Gust loads on aircraft:Concepts and applications[M]. Reston:AIAA, 1988:1-14.
[10] ROSKAM J, DUSTO A. A method for predicting longitudinal stability derivatives of rigid and elastic airplanes[J]. Journal of Aircraft, 1969, 6(6):525-531.
[11] RODDEN W P. Dihedral effect of a flexible wing[J]. Journal of Aircraft, 1965, 2(5):368-373.
[12] LIVNE E. Aircraft active flutter suppression:State of the art and technology maturation needs[J]. Journal of Aircraft, 2017, 55(1):410-452.
[13] RODDEN W P, GIESING J P. Application of oscillatory aerodynamic theory to estimation of dynamic stability derivatives[J]. Journal of Aircraft, 1970, 7(3):272-275.
[14] 杨超. 飞行器气动弹性原理[M]. 2版. 北京:北京航空航天大学出版社, 2016:1-164. YANG C. Aeroelastic principle of aircraft[M]. 2nd ed. Beijing:Beijing University of Aeronautics & Astronautics Press, 2016:1-164(in Chinese).
[15] BISPLINGHOFF R L, ASHLEY H. Principles of aeroelasticity[M]. New York:Dover Publications, 2013:18-70.
[16] MILNE R D. Dynamics of the deformable aeroplane. Part 1. The equations of motion. Part 2. A study of the trim state and longitudinal stability of the slender integrated aeroplane configuration[R]. London:Aeronautical Research Council, 1964.
[17] WASZAK M, BUTTRILL C, SCHMIDT D. Modeling and model simplification of aeroelastic vehicles:An overview:NASA-TM-107691[R]. Washington,D.C:NASA, 1992.
[18] WASZAK M R, SCHMIDT D K. Flight dynamics of aeroelastic vehicles[J]. Journal of Aircraft, 1988, 25(6):563-571.
[19] SCHMIDT D K, RANEY D L. Modeling and simulation of flexible flight vehicles[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(3):539-546.
[20] BUTTRILL C, ARBUCKLE P, ZEILER T. Nonlinear simulation of a flexible aircraft in maneuvering flight[C]//Flight Simulation Technologies Conference. Reston:AIAA, 1987.
[21] KOKOTOVIĆ P V, O'MALLAY R E Jr, SANNUTI P. Singular perturbations and order reduction in control theory-An overview[J]. Automatica, 1976, 12(2):123-132.
[22] MEIROVITCH L, TUZCU I. Integrated approach to flight dynamics and aeroservoelasticity of whole flexible aircraft-part I:system modeling[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston:AIAA, 2002.
[23] MEIROVITCH L, TUZCU I. Integrated approach to the dynamics and control of maneuvering flexible aircraft:NASA/CR-2003-211748[R]. Washington, D.C.:NASA, 2003.
[24] MEIROVITCH L, TUZCU I. Time simulations of the response of maneuvering flexible aircraft[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(5):814-828.
[25] MEIROVITCH L, TUZCU I. Unified theory for the dynamics and control of maneuvering flexible aircraft[J]. AIAA Journal, 2004, 42(4):714-727.
[26] NOLL T, ISHMAEL S, HENWOOD B, et al. Technical findings, lessons learned, and recommendations resulting from the helios prototype vehicle mishap:NASA/WBS-810031[R]. Washington, D.C.:NASA, 2007.
[27] HODGES D, DOWELL E. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades:NASA TN D-7818[R]. Washington, D.C.:NASA, 1974.
[28] HODGES D H, ORMISTON R A, PETERS D A. On the nonlinear deformation geometry of Euler-Bernoulli beams:NASA-1566[R]. Washington, D.C.:NASA, 1980.
[29] HINNANT H E, HODGES D H. Nonlinear analysis of a cantilever beam[J]. AIAA Journal, 1988, 26(12):1521-1527.
[30] HODGES D H. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams[J]. International Journal of Solids and Structures, 1990, 26(11):1253-1273.
[31] ATILGAN A R, HODGES D H. Unified nonlinear analysis for nonhomogeneous anisotropic beams withclosed cross sections[J]. AIAA Journal, 1991, 29(11):1990-1999.
[32] CESNIK C E S, HODGES D H, SUTYRIN V G. Cross-sectional analysis of composite beams including large initial twist and curvature effects[J]. AIAA Journal, 1996, 34(9):1913-1920.
[33] PATIL M, HODGES D, CESNIK C. Nonlinear aeroelastic analysis of aircraft with high-aspect-ratio wings[C]//39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston:AIAA, 1998.
[34] PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelastic analysis of complete aircraft in subsonic flow[J]. Journal of Aircraft, 2000, 37(5):753-760.
[35] PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft[J]. Journal of Aircraft, 2001, 38(1):88-94.
[36] PATIL M J, HODGES D H. Flight dynamics of highly flexible flying wings[J]. Journal of Aircraft, 2006, 43(6):1790-1799.
[37] PATIL M, TAYLOR D. Gust response of highly flexible aircraft[C]//47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 14th AIAA/ASME/AHS Adaptive Structures Conference. Reston:AIAA, 2006.
[38] PATIL M. Nonlinear gust response of highly flexible aircraft[C]//48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston:AIAA, 2007.
[39] HOUBOLT J C. Design manual for vertical gusts based on power spectral techniques:AFFDL-TR-70-106[R]. Princeton:Aeronautical Research Associates of Princeton Inc, 1970.
[40] 金长江, 肖业伦. 大气扰动中的飞行原理[M]. 北京:国防工业出版社, 1992:11-70. JIN C J, XIAO Y L. Flight principle in atmospheric disturbance[M]. Beijing:National Defense Industry Press, 1992:11-70(in Chinese).
[41] FULLER J R. Evolution of airplane gust loads design requirements[J]. Journal of Aircraft, 1995, 32(2):235-246.
[42] FAA. Federal aviation regulations, Part25:airworthiness standards:transport category airplanes, Section 341:Gust and turbulence loads[S]. Washington, D.C.:Department of Transportation, Federal Aviation Administration, 1996.
[43] EASA. Certification specifications for large aeroplanes:CS-25[S]. Europe:EASA, 2009.
[44] CAA. Joint airworthiness requirements, JAR-25:Large aeroplanes[S]. Cheltenham:Civil Aviation Authorities, 1994.
[45] 中国民用航空局. CCAR-25-R4中国民用航空规章第25部:运输类飞机适航标准[S]. 北京:中国民用航空局, 2016. Civil Aviation Administration of China. CCAR-25-R4 China Civil Aviation Regulations Part 25:Airworthiness standards for transport aircraft[S]. Beijing:Civil Aviation Administration of China, 2016(in Chinese).
[46] FULLER J, FULLER J. Evolution and future development of airplane gust loads design requirements[C]//1997 World Aviation Congress. Reston:AIAA, 1997.
[47] WU Z, CAO Y, ISMAIL M. Gust loads on aircraft[J]. The Aeronautical Journal, 2019, 123(1266):1216-1274.
[48] NOBACK R. Comparison of discrete and continuous gust methods for airplane design loads determination[J]. Journal of Aircraft, 1986, 23(3):226-231.
[49] JONES J G. Modelling of gusts and wind shear for aircraft assessment and certification[J]. Proceedings of the Indian Academy of Sciences Section C:Engineering Sciences, 1980, 3(1):1-30.
[50] YANG Y, YANG C, WU Z G. Aeroelastic dynamic response of elastic aircraft with consideration of two-dimensional discrete gust excitation[J]. Chinese Journal of Aeronautics, 2020, 33(4):1228-1241.
[51] 杨超, 黄超, 吴志刚, 等. 气动伺服弹性研究的进展与挑战[J]. 航空学报, 2015, 36(4):1011-1033. YANG C, HUANG C, WU Z G, et al. Progress and challenges for aeroservoelasticity research[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(4):1011-1033(in Chinese).
[52] 杨超, 杨澜, 谢长川. 大展弦比柔性机翼气动弹性分析中的气动力方法研究进展[J]. 空气动力学学报, 2018, 36(6):1009-1018, 983. YANG C, YANG L, XIE C C. Development of aerodynamic methods in aeroelastic analysis for high aspect ratio flexible wings[J]. Acta Aerodynamica Sinica, 201

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