一体化试验评估在美国飞行器研制中的应用

何磊; 张天姣; 钱炜祺; 周宇; 邵元培

doi:10.7638/kqdlxxb-2019.0035

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一体化试验评估在美国飞行器研制中的应用

研究论文 | 更新时间：2026-05-28

- 一体化试验评估在美国飞行器研制中的应用
- Application of integrated test and evaluation in the development of aircraft in America
- 空气动力学学报 2020年38卷第3期页码：461-469
- 作者机构：
  
  中国空气动力研究与发展中心,绵阳,621000
- 作者简介：
  
  何磊(1988-), 男, 四川绵竹人, 博士, 助理研究员, 研究方向:飞行器建模与仿真.E-mail:helei_email@163.com
  钱炜祺(1973-), 男, 江苏无锡人, 博士, 研究员, 研究方向:气动/飞行试验数据分析与评估.E-mail:qwqhyy@sina.com
- 基金信息：
  
  中国空气动力研究与发展中心基础和前沿技术研究基金（FFTRF20172015）
- DOI：10.7638/kqdlxxb-2019.0035
  中图分类号： V37
- 纸质出版：2020
- 稿件说明：
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何磊, 张天姣, 钱炜祺, 周宇, 邵元培. 一体化试验评估在美国飞行器研制中的应用[J]. 空气动力学学报, 2020, 38(3): 461-469.

HE Lei, ZHANG Tianjiao, QIAN Weiqi, et al. Application of integrated test and evaluation in the development of aircraft in America[J]. 2020, 38(3): 461-469.
何磊, 张天姣, 钱炜祺, 周宇, 邵元培. 一体化试验评估在美国飞行器研制中的应用[J]. 空气动力学学报, 2020, 38(3): 461-469. DOI： 10.7638/kqdlxxb-2019.0035.

HE Lei, ZHANG Tianjiao, QIAN Weiqi, et al. Application of integrated test and evaluation in the development of aircraft in America[J]. 2020, 38(3): 461-469. DOI： 10.7638/kqdlxxb-2019.0035.

摘要

一体化试验评估是从分系统、研制过程、研究手段三个维度来对飞行器各研制阶段的试验活动进行统筹规划和组织实施的方法，可以有效提高试验效率、缩短试验周期、减少试验成本并降低试验风险。文章在剖析美国提出的飞行器一体化试验评估内涵的基础上，介绍了一体化试验评估方法在飞行器外挂物投放、航空推进系统、高超声速武器系统以及无人机系统中的应用情况，分析了一体化试验评估应用于飞行器研制中的除地面风洞试验和飞行试验外的其他相关关键技术，并从大数据和人工智能、高性能计算、体系分析、人类行为建模四个方面对其后续发展趋势进行了展望，最后总结了一体化试验评估在美国飞行器研制中落地的原因和对我国应用的启示。

Abstract

Integrated test and evaluation (ITE) is an approach to support system development from three dimensions:subsystem

development process

and research methods. It can improve test efficiency

shorten development cycle

cut down test cost

and reduce test risk. Firstly

this paper reviews the development history of integrated test and evaluation concept

and demonstrates how the concept is applied to the development of an aircraft system from a system of systems viewpoint. Then

the application of integrated test and evaluation in flight store separation and propulsion systems test project of AEDC

the development of hypersonic weapon system project of USAF

and the "Unmanned Aircraft Systems Integration in the National Airspace System" project of NASA are introduced. Next

the relevant key technologies include test design

data management

modeling and simulation are analyzed except ground wind tunnel test and flight test

and the future development trend is prospected from four aspects:big data and artificial intelligence

high performance computing

system of systems

and human behavior modeling. Finally

the reasons why the United States can proposed the integrated test and evaluation concept firstly and successfully applied it to aircraft development are analyzed.

关键词

Keywords

references

WEST T D. Reinvigorating technical rigor in test, evaluation and analyses at the Arnold Engineering Development Complex-A retrospective on ten years of progress[C]//34th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Atlanta, Georgia, USA, 2018. AIAA 2018-2923.

KRAFT E M. Integrated test and Evaluation-A Knowledge-based approach to system development[C]//Aircraft Engineering, Technology, and Operations Congress, Los Angeles, CA, USA, 1995. AIAA 95-3982, 1995. https://doi.org/10.2514/6.1995-3982

BENEK J A, LANGHAM T F, JR BAKER W B. Historical perspective on the integration of testing and evaluation methodologies at the Arnold Engineering Development Center[C]//25th Plasmadynamics and Lasers Conference, Colorado Springs, CO, USA. Reston, Virigina: AIAA, 1994. AIAA 1994-2470. https://doi.org/10.2514/6.1994-2470

WATERS M D P. Integrating modeling and simulation with test and evaluation activities[C]//USAF Developmental Test and Evaluation Summit, Woodland Hills, California, 2004. AIAA 2004-6800. https://doi.org/10.2514/6.2004-6800

SKELLEY M L, LANGHAM T F, PETERS W L. Integrated test and evaluation for the 21st century[C]//USAF Developmental Test and Evaluation Summit, Woodland Hills, California, 2004. AIAA 2004-6873. https://doi.org/10.2514/6.2004-6873

KIM J H, LEE I W, YANG H D. Integrated test and evaluation approach to improve aircraft store separation[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, California, 2005. AIAA 2005-6223. https://doi.org/10.2514/6.2005-6223

CENKO A. Lessons learned in 30 years of store separation testing[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, 2009. AIAA 2009-0098. https://doi.org/10.2514/6.2009-98

YANG L, WU X Y. Technical progress of US equipments integrated test and evaluation[J]. National Defense Science and Technology, 2010, 31(2):8-14. (in Chinese)

ZHANG B Z. Study on integrated test and evaluation strategy and its applications in the development of US weapon systems[J]. Measurement Control Technology, 2007, 26(3):8-10. (in Chinese)

Deputy Secretary of Defense. DoDI 5000.02: Operation of the defense acquisition system[M]. Washington: Department of Defense, 2008.

DARLENE M K. Test and evaluation policies and practices:A new emphasis[J].ITEA Journal, 2008, 29:157-159.

BIXBY C J. Integrated tests and evaluations[C]//Meeting of Experts on NASA's Unmanned Aircraft System (UAS) Integration in the National Airspace Systems (NAS) Project. Aeronautics and Space Engineering Board, National Research Council, 2010. N20100027490.

LABEL K A, COHN L M. Radiation testing and evaluation issues for modern integrated circuits[R]. RADECS2005, NASA Technical Reports Server, 2005. N20050243591.

LEI S, DING S M. Discussion of the development law of test and evaluation based on integrated test and evaluation[J]. National Defense Science and Technology, 2011, 32(4):36-39. (in Chinese)

Defense Acquisition University. Test and evaluation management guide(sixth edition)[M]. Virginia:The Defense Acquisition University Press, 2012:23.

ERNO J L. Air force development test and evaluation under acquisition reform: six flight test process concepts[M]. BiblioScholar, 2012. ISBN-10: 1286861616, ISBN-13: 978-1286861615

BEI B X. Integrated test and evaluation of U.S. equipment: integrated knowledge and action[EB]. Strategic Management and Assessment, 2016-03-10. (in Chinese)

DAVIS M W, HALE A A, KLEPPER J, et al. Demonstration of an Integrated Test and Evaluation (ITE) process for airframe-propulsion systems as applied to a current weapon system program[C]//48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, rlando, Florida, 2010. AIAA 2010-1039. https://doi.org/10.2514/6.2010-1039

SKELLEY M, LANGHAM T, PETERS W, et al. Lessons learned during joint strike fighter ground testing and evaluation at AEDC[C]//2007 U.S. Air Force T&E Days, Destin, Florida, 2007. Reston, Virigina: AIAA. AIAA 2007-1635. https://doi.org/10.2514/6.2007-1635

PETERS W L, LANGHAM T F, SKELLEY M L. T&E lessons learned from wind tunnel testing of the B-1 A/B bomber in preparation for next-generation long-range strike (NGLRS) development[C]//2008 U.S. Air Force T&E Days, Los Angeles, California, 2008. Reston, Virigina: AIAA. AIAA 2008-1619 https://doi.org/10.2514/6.2008-1619

JR BAKER W B, KEEN S, MORGRET C. Validation of weapon separation predictions using F/A-22 flight test results[C]//USAF Developmental Test and Evaluation Summit, Woodland Hills, California, 2004. Reston, Virigina: AIAA. AIAA 2004-6803. https://doi.org/10.2514/6.2004-6803

凌静, 臣墨. NASA成功开展无人机系统融入国家空域系统(UAS-NAS)项目第三阶段飞行试验[J].飞航导弹, 2015, (10):2.

LEE J M, DUNWORTH K S, RIZK M, et al. Studies of combined use of CFD and wind tunnel test approaches to simulate a store separation from F-15E using efficient CFD database generation[C]//22nd Applied Aerodynamics Conference and Exhibit, Providence, Rhode Island, 2004. Reston, Virigina: AIAA. AIAA 2004-4724. https://doi.org/10.2514/6.2004-4724

LIU L Q, ZHANG Q, LIU H. Weapon separation modeling simulation and test of F/A-22 stealth fighter[J]. Journal of Ordnance Equipment Engineering, 2016, 37(10):8-12.(in Chinese)

YIN C S, LEI W T. Investigation of wind tunnel and flight correlation research ideas on external-store drop[J]. Aeronautical Science and Technology, 2015, 26(3):14-18. (in Chinese)

ZHOU N C, LI B, ZHENG M, et al. Missile separation simulation with control laws[J]. Acta Aerodynamica Sinica, 2013, 31(3):288-293. (in Chinese)

JIANG Z H, SONG W, LU W, et al. Critical problems and applied fields of drop-model testing technique in high speed wind tunnel[J]. Acta Aerodynamica Sinica, 2016, 34(6):744-749, 802. (in Chinese)

CAI G H. Researches of experimental techniques about dropping test of External stores in the low speed wind tunnel[J]. Acta Aerodynamica Sinica, 1999, 17(4):477-483. (in Chinese)

TANG Z G, LI B, ZHENG M, et al. Store separation simulation using overset unstructured grid[J]. Acta Aerodynamica Sinica, 2009, 27(5):592-596. (in Chinese)

CRASSIDIS A L. Identification update of aerodynamic models with sensor consistency checks[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2004. Providence, Rhode Island. AIAA 2004-5062. https://doi.org/10.2514/6.2004-5062

Jr MILT W D, HALE A A, KLEPPER J. 40 years of AEDC development, evolution and application of numerical simulations for integrated test and evaluation of turbine engine turbomachinery operability issues[R]. AEDC-TR-09-T-19, 2010.

TIAN J M, JING J B, HAN G Q. Overview on hypersonic aircraft ground test method[J]. Journal of Detection Control, 2013, 35(5):57-60. (in Chinese)

FETTERHOFF T, KRAFT DR E, LASTER DR M L, et al. High-speed/hypersonic test and evaluation infrastructure capabilities study[C]//14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, Canberra, Australia, 2006. AIAA 2006-8043. https://doi.org/10.2514/6.2006-8043

胡冬冬, 叶蕾.从高速系统试验(HSST)项目看美国高超声速试验科学技术专项实施现状[J].飞航导弹, 2016, (4):22-27.

MARSTON M L. Integrated test and evaluation flight test 3 flight test plan[R]. NASA, DFRC-E-DAA-TN22417, 2015.

MARSTON M L. Integrated Test and Evaluation(ITE) flight test series 4[R]. NASA, DFRC-E-DAA-TN39175, 2015.

MALISKA H. Unmanned Aircraft Systems (UAS) Integration in the National Airspace System (NAS) Project: integrated test and evaluation flight testing overview[R]. NASA Armstrong Flight Research Center, 2017. AFRC-E-DAA-TN43574.

KLEPPER J, KNAPKE R, SIRBAUGH J, et al. Computational modeling and simulation applications to support integrated test and evaluation (ITE) at AEDC[C]//2018 Aerodynamic Measurement Technology and Ground Testing Conference, Atlanta, Georgia. Reston, Virginia: AIAA. AIAA 2018-3873. https://doi.org/10.2514/6.2018-3873

KNAPKE R, MASTERS J, TATUM K, et al. AEDC computational modeling and simulation support to integrated test and evaluation[C]//55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, 2017. AIAA 2017-0272.

WANG P, LI G, HUANG K D. Architecture and time management for integrated simulation of infield and outfield[J]. Systems Engineering and Electronics, 2017, 39(10):2255-2263. (in Chinese)

GUSTAVSSON PER M, BJÖRKMAN ULF, WEMMERGÅRD J. LVC aspects and integration of live simulation[C]//Fall Simulation Interoperability Workshop (FallSIW 2009), Orlando, FL, USA, 2009.

CHEN X X, XU L, QU K, et al. Research on simulation architecture development state and trends[J]. Computer Engineering and Applications, 2014, 50(9):32-36, 40. (in Chinese)

XUE F X, YAO Y P, LI D. Application of DIS in weapon systems test and evaluation[J]. Computer Simulation, 2005, 22(2):35-37. (in Chinese)

谢文苗.复杂系统仿真关键技术研究[D].北京: 北京理工大学, 2015.

XU Z F, WANG G Y, ZHANG Y Z, et al. Progresses and Prospects of TENA[J]. Journal of System Simulation, 2008, 20(23):6325-6329. (in Chinese)

FENG R M, WANG G Y, HUANG K D. TENA and its comparison with HLA[J]. Systems Engineering and Electronics, 2005, 27(2):288-291. (in Chinese)

王西宝.武器装备联合仿真试验关键技术研究[D].长沙: 国防科学技术大学, 2017.

石实, 曹裕华.美军武器装备体系试验鉴定发展现状及启示[J].军事运筹与系统工程, 2015, 29(3):46-51.

VADDI S S, NGUYEN J, MENON P, et al. Data mining and knowledge discovery from store separation trajectories[C]//AIAA Atmospheric Flight Mechanics Conference, Chicago, Illinois, 2009. AIAA 2009-5732. https://doi.org/10.2514/6.2009-5732

MORRIS C C, CROWLEY D R. Uncertainty propagation via Monte Carlo simulation in the PWT and VKF wind tunnels at AEDC[C]//32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Washington, D.C., 2016. AIAA 2016-3500. https://doi.org/10.2514/6.2016-3500

LINE W B. Proven Cost Savings by Using Modern Design of Experiments(MDOE)[C]//48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, 2010. AIAA 2010-0081. https://doi.org/10.2514/6.2010-81

涂亿彬. LVC联合试验体系架构及关键技术研究[D].长沙: 国防科学技术大学, 2016.

CHEN L X. Thoughts on the equipments contribution rate to system of systems[J]. Military Operations Research and Systems Engineering, 2018, 32(3):37-43. (in Chinese)

TUTTY M G, AKROYD G, CENKO A, et al. Stores separation from weapons bays[C]//30th Congress of the ICAS, Daejeon, Korea, 2016. ICAS 2016-0156.

LI X B, LIN M, SHU Z, et al. Synthesized capability-effectiveness evaluation method of contribution ratio to system-of-systems[J]. Journal of System Simulation, 2018, 30(12):4520-4528, 4535. (in Chinese)

南生今世说. 2018年研发投入: 美国第1、日本第3、德国第4、印度第6, 那中国呢?[EB].搜狐网, 2019-02-15.http://www.sohu.com/a/293441629_100110525

韩洪涛.从经费预算看美国高超声速领域发展趋势[J].中国航天, 2016(6):30-34.

席亚洲.美国高超声速投资将增10倍, 为什么才开始?[EB].观察者网, 2019-03-14.https://user.guancha.cn/main/content?id=89044&s=fwzxfbbt

WANG X, LI F. Research on several issues in test and evaluation[J]. Journal of Academy of Equipment, 2017, 28(2):84-87. (in Chinese)

见证中国首颗原子弹爆炸, 一级专列运送原子弹[EB].中国新闻网, 2012-06-26.http://www.chinanews.com/mil/2012/06-26/3987056.shtml

HE YY, HE W, ZHANG X Q, et al. Aero-propulsion integration test in combustion heated impulse facility[J]. Journal of propulsion technology, 2017, 38(8):66-71. (in Chinese)

DU Z B, JING Z, CHEN J Z. Integrated test and evaluation technology of hit accuracy for laser-guide missile[J]. Aeronautical Science Technology, 2019, 30(3):75-78. (in Chinese)

ZHAO X C, SHI W K. Simulation and flight test integration technique in missile finalized test and evaluation[J]. Modern Defence Technology, 2012, 40(6):150-154. (in Chinese)

LYU Y G, LUO G H. The status and development of equipment flight test mode[J]. National Defense Science Technology, 2016, 37(1):100-105. (in Chinese)

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