Components and Subsystems Design and Others

Probability-based risk analysis of hypersonic vehicle systems engineering

  • SHEN Zuojun ,
  • LIU Qing ,
  • XIAO Jiaping
Expand
  • 1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China;
    2. The Third Research Institute, China Aerospace Science and Technology Corp., Beijing 100074, China

Received date: 2015-10-19

  Revised date: 2015-11-22

  Online published: 2015-12-04

Abstract

Different risks associated with decision party and system developer are modeled and analyzed aiming at the high risk characteristics of hypersonic vehicle development.Based upon the inherent probabilistic risks of system design and critical technologies,a generic test and verification process is adopted to calculate the probabilities of accepting unqualified systems by the decision party,or over-testing low risk systems or technologies by the developer.The relation between decision risk and developer's risk is studied,and then a system engineering approach for balancing the risks as well as optimizing the development cycle is proposed based on probability calculation.

Cite this article

SHEN Zuojun , LIU Qing , XIAO Jiaping . Probability-based risk analysis of hypersonic vehicle systems engineering[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016 , 37(1) : 317 -323 . DOI: 10.7527/S1000-6893.2015.0316

References

[1] 张蒙正,邹宇.美国典型高超飞行器项目研发及启示[J].火箭推进,2012,38(2):1-8.ZHANG M Z,ZOU Y.Development of American typical hyper-sonic flight vehicles and its enlightenment[J].Journal of Rocket Propulsion,2012,38(2):1-8(in Chinese).
[2] NASA Systems Engineering Handbook.NASA center for aerospace information:NASA/SP-2007-6105[R].Washington,D.C.:NASA,2007:15-35.
[3] GRINFFIN M D.System engineering and the "Two cultures" of engineering(Boeing lecture presented at Purdue University)[R].Lafayette:Purdue University,2007:1-3.
[4] 徐志磊.以科学为基础的复杂系统工程研制[J].中国工程科学,2002,4(10):1-12.XU Z L.Science-based engineering R & D of complex systems[J].Engineering Science,2002,4(10):1-12(in Chinese).
[5] GRAVES R E.An analytics-based methodology for assessing aerospace system uncertainty to augment risk-informed systems engineering processes:AIAA-2013-0723[R].Reston:AIAA,2013.
[6] 余后满,林益明,陈虎,等.航天器系统方案设计模式研究[J].航天器工程,2010,19(3):1-6.YU H M,LIN Y M,CHEN H,et al.Improved mode for spacecraft system scheme design[J].Spacecraft Engineering,2010,19(3):1-6(in Chinese).
[7] SOLISH B,COOKE B,COX N,et al.Verification & validation by risk class:Understanding how risk classes affect the V & V process:AIAA-2013-5527[R].Reston:AIAA,2013.
[8] LUM C W,WAGGONER B.A risk based paradigm and model for unmanned aerial systems in the national airspace:AIAA-2011-1424[R].Reston:AIAA,2011.
[9] PATRIC S,SHAWN G,TIM G.Probabilistic risk analysis methodology on inadvertent laser illumination of satellite optical systems[J].Journal of Spacecraft and Rockets,2014,51(6):1994-2007.
[10] GAMBLE K B,LIGHTSEY E G.Decision analysis applied to small satellite risk management:AIAA-2015-1863[R].Reston:AIAA,2015.
[11] JIMENEZ H,SCHUTTE J,MAVRIS D.System readiness and risk assessment for advanced vehicle concepts-discussion of fundamental concepts:AIAA-2011-0423[R].Reston:AIAA,2011.
[12] 沈小明,张彤,揭裕文.航空产品研制阶段的技术性能风险研究[J].南京航空航天大学学报(社会科学版),2014,16(1):64-71.SHEN X M,ZHANG T,JIE Y W.Research on technical performance risk during aero-product development[J].Journal of Nanjing University of Aeronautics & Astronautics(Social Sciences),2014,16(1):64-71(in Chinese).
[13] 徐哲,冯允成,鲁大伟.武器装备研制项目的技术风险评估[J].系统工程与电子技术,2005,27(6):1123-1127.XU Z,FENG Y C,LU D W.Appraisement model of technical risk for weapon system development[J].Systems Engineering and Electronics,2005,27(6):1123-1127(in Chinese).
[14] SIEVERS M,MADNI A M.Defining "Credible Faults," a risk-based approach:AIAA-2015-4528[R].Reston:AIAA,2015.
[15] ENRIGHT M P,LIANG W W.Development of risk contours for assessment of aircraft engine components:AIAA-2010-2846[R].Reston:AIAA,2010.
[16] BOUDALI H,SáNCHEZ A H.A conceptual design phase risk assessment methodology for space-based system of systems:AIAA-2010-8738[R].Reston:AIAA,2010.
[17] HAMLIN T L,THIGPEN E,KAHN J,et al.Shuttle risk progression:Use of the shuttle probabilistic risk assessment(PRA) to show reliability growth:AIAA-2011-7353[R].Reston:AIAA,2011.
[18] 赵净净.民用飞机研发过程中的权衡研究[J].科技创新导报,2011(34):5-14.ZHAO J J.Trade study of civil aircraft development [J].Science and Technology Innovation Herald,2011(34):5-14(in Chinese).
[19] HANSON J M,BEARD B B.Applying monte carlo simulation to launch vehicle design and requirements verification[J].Journal of Spacecraft and Rockets,2012,49:136-144.
[20] 盛骤,谢式千,潘承毅.概率论与数理统计[M].北京:高等教育出版社,2001:25-145.SHENG Z,XIE S Q,PAN C Y.Probability theory and mathematical statistics[M].Beijing:Higher Education Press,2001:25-145(in Chinese).

Outlines

/