항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제11권3호
  • /
  • Pages.22-30
  • /
  • 2017
  • /
  • 1976-6300(pISSN)
  • /
  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
권호 표지
DOI QR코드

DOI QR Code

중국의 연구 사례를 통한 개방형 액체로켓엔진의 고장진단 동향 분석

A Survey on Fault Detection and Diagnosis Method for Open-Cycle Liquid Rocket Engines through China R&D Case

  • 이계림 (한국항공대학교 항공우주 및 기계공학과) ;
  • 차지형 (한국항공대학교 항공우주 및 기계공학과) ;
  • 고상호 (한국항공대학교 항공우주 및 기계공학과)
  • Lee, Kyelim (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Cha, Jihyoung (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Ko, Sangho (Department of Aerospace and Mechanical Engineering, Korea Aerospace University)
  • 투고 : 2017.02.13
  • 심사 : 2017.05.30
  • 발행 : 2017.06.30
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

본 논문은 액체로켓엔진의 건전성 감시 및 관리기법에 대한 연구 동향을 소개한다. 이를 위하여 실제 액체로켓엔진에 연구 및 적용되었던 고장진단 알고리즘을 조사하였다. 특히 한국형발사체(Korea Space Launch Vehicle II, KSLV-II)에 적용하기 위해 한국형발사체 로켓엔진과 같은 구조인 개방형 액체로켓 엔진에 적용된 알고리즘을 조사하였다. 이러한 과정을 통해 적용된 사례들의 특징을 따로 세분화하고, 한국형발사체 로켓엔진과 비슷한 중국의 개방형 액체로켓엔진들의 고장진단 기법 특징들을 분석하였다. 나아가 2019년에 발사를 목표로 하는 한국형발사체에 적용시키기 위해 고려해야 할 사항에 대하여 토론하고자 한다.

This paper examines a survey on recent research regarding health monitoring and management for liquid rocket engines (LRE). For this, we investigated precedent techniques applied to LRE development. Particularly, we focused on open-cycle LRE to apply to KSLV-II (Korea Space Launch Vehicle II). Through this study, we subdivided health monitoring algorithms and analyzed fault detection and diagnosis algorithm developed in China, since China researched open-cycle LRE that have the same cycle as KSLV-II rocket engines. We discuss significant points to be considered regarding development of the KSLV-II.

키워드

참고문헌

  1. J. H. Cha, C. S. Ha, S. H. O and S. H. Ko, "A Survey on Health Monitoring and Management Technology for Liquid Rocket Engines," Journal of The Korean Society of Propulsion Engineers, vol. 18, no. 6, pp. 50-58, 2014. https://doi.org/10.6108/KSPE.2014.18.6.050
  2. I. S. Chang, "Space Launch Vehicle Reliability," World Wide Web location http://aerospace.wpengine.netdna-cdn.com/wp-content/uploads/crosslink/V6N2.pdf, pp. 22-32, 2005.
  3. J. H. Choi, "A review on prognostics and health management and its applications," Journal of The Society for Aerospace System Engineering, vol. 8, no. 4, pp. 7-17, 2014.
  4. C. W. Kim, S. Y. Park and W. K. Cho, "Methodology of Liquid Rocket Engine Diagnosis," Korea Aerospace Technology, vol. 11, no. 2, pp. 182-194, 2012.
  5. C. W. Kim, S. H. Kim, C. H. Nam and W. S. Seol, "Reduction of the Accident Risk of Liquid Rocket Engine," Proc. of 31st KSPE Fall Conference, pp. 388-392, 2008.
  6. I. S. Kim and E. S. Lee, "Recent Trends in Liquid Rocket Engine Health Monitoring/Management Methods," Proc. of 32nd KSPE Fall Conference, pp. 824-832, 2012.
  7. C. W. Kim, S. Y. Park and W. K. Cho, "Flight Test Preparation for Liquid Rocket Engine and Its Diagnosis," Proc. of 31st KSPE Fall Conference, pp. 34-39, 2013.
  8. M. Son and J. Y. Koo, "One Dimensional Analysis for Dynamic Characteristics of Turbopump-fed Liquid Rocket Engine," Journal of The Society for Aerospace System Engineering, vol. 4, no. 1, pp. 1-9, 2010.
  9. J. H. Cha, C. S. Ha, J. Y. Koo and S. H. Ko, "Dynamic Simulation and Analysis of the Space Shuttle Main Engine with Artificially Injected Faults," International Journal of Aeronautical and Space Sciences, vol. 17, no. 4, pp. 535-550, 2016. https://doi.org/10.5139/IJASS.2016.17.4.535
  10. J. H. Cha, C. S. Ha, S. H. Ko and J. Y. Koo, "Application of fault factor method to detection and diagnosis for space shuttle main engine," Acta Astronautica, vol.126, pp. 517-527, 2016. https://doi.org/10.1016/j.actaastro.2015.12.024
  11. H. V. Panossian and W. D. Ewing, "Real-time failure detection algorithm for the space shuttle main engine," IEEE Control System, vol. 17, no. 4, pp. 16-23, 1997.
  12. T. W. Bickmore and R. L. Bickford, "Aerojet's Titan health assessment expert system," Proc. of the 28th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Nashville, TN, AIAA-92-3330, Jul. 1992.
  13. C. F. Lorenzo and J. L. Musgrave, "Overview of rocket engine control," NASA, TM-105318, Jan. 1992.
  14. B. Katorgin, F. Chelkis and C. Limerick, "The RD-170, a different approach to launch vehicle propulsion," Proc. of the 29th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Monterey, CA, AIAA-93-2415, Jun. 1993.
  15. N. Goncharov, V. Orlov, A. Shostak and R. Starke, "Reusable launch vehicle propulsion based on the RD-0120 Engine," Proc. of the 31st AIAA/ASME /SAE/ASEE Joint Propulsion Conference, SanDiego, CA, AIAA-95-3003, Jul. 1995.
  16. Y. Zichu, "The development of condition monitoring and failure diagnostic technique for liquid propellant rocket engines," Missiles and Space Vehicles of China, no. 2, pp. 8-17, 1994.
  17. J. Wu, Y. Zhang and Q. Chen, "Transient performance simulation of a large liquid rocket engine under fault condition," Journal of Aerospace Power of China, vol. 9, no. 4, pp. 361-365, 1994.
  18. J. Wu, Y. Zhang and Q. Chen, "Steady fault simulation and analysis of liquid rocket engine," Journal of Propulsion Technology of China, vol. 15, no. 3, pp. 6-13, 1994.
  19. J. Wu, Y. Zhang and Q. Chen, "A real-time verification system on fault diagnosis methods for liquid propellant rocket engine," Proc. of the 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FL, AIAA-96-2831, Jul. 1996.
  20. J. Wu, Y. Zhang and Q. Chen, "Real-time fault detection algorithm based on neural networks for liquid propellant rocket engine," Proc. of the 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FL, AIAA-96-2591, Jul. 1996.
  21. J. Wu, Y. Zhang and Q. Chen, "Real-time on-line fault detection algorithm for starting process of liquid propellant rocket engines," Journal of Propulsion Technology of China, vol. 17, no. 6, pp.24-57, 1996.
  22. Y. Zhang, J. Wu, M. Huang, H. Zhu and Q. CHen, "Liquid-propellant rocket engine health-monitoring techniques," Journal of Propulsion and power, vol. 14, no. 5, pp. 657-663, 1998. https://doi.org/10.2514/2.5327
  23. S. Yuan and F. Chu, "Fault diagnosis based on support vector machines with parameter optimisation by artificial immunisation algorithm," Mechanical System and Signal Processing, vol. 21, no. 3, pp. 1318-1330, 2007. https://doi.org/10.1016/j.ymssp.2006.06.006
  24. W. Dou and Z. S. Liu, "A new fault diagnosis method for turbopump of liquid rocket engine," Journal of Propulsion Technology of China, vol. 32, no. 2, pp.266-270, 2011.
  25. H. Liu, T. Xie, Q. Huang and J. Wu, "Real-time fault detection and alarm system for ground test of liquid propellant rocket engines," Missiles and Space Vehicles of China, no. 1, pp.49-52, 2008.
  26. Y. Zhang, D. Wang and H. Sha, "Application of kalman filter adaptive algorithm to the fault detection of a liquid missile power system," Mechanical Science and Technology of China, vol. 25, no. 7, pp.789-792, 2006.
  27. B. Long, L. Song, W. Jing, Z. Jiang and Z. Li, "A review and propect of fault diagnosis technique of spacecrafts," Missiles and Space Vehicles of China, no. 3, pp.32-37, 2003.
  28. J. Wu, Y. Zhang and Q. Chen, "Health monitoring techniques for liquid rocket engine - a survey," Journal of Astronautics of China, vol. 16, no. 2, pp. 93-99, 1995.