한국추진공학회지 (Journal of the Korean Society of Propulsion Engineers)

  • 제20권1호
  • /
  • Pages.28-36
  • /
  • 2016
  • /
  • 1226-6027(pISSN)
  • /
  • 2288-4548(eISSN)
한국추진공학회 (The Korean Society of Propulsion Engineers)
권호 표지
DOI QR코드

DOI QR Code

가변 추력 고체추진기관의 추력 제어를 위한 이득 계획 제어기 설계 및 성능 분석

Gain Scheduling Controller Design and Performance Evaluation for Thrust Control of Variable Thrust Solid Rocket Motor

  • Hong, SeokHyun (The 4th R&D Institute, Agency for Defense Development)
  • 투고 : 2015.05.04
  • 심사 : 2016.01.06
  • 발행 : 2016.02.01
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

본 논문에서는 핀틀을 이용한 가변추력 고체 추진기관의 추력을 제어하기 위하여 이론적으로 모델을 구하고 압력 제어기를 설계하였다. 고전적인 모델 선형화 및 비례-적분제어를 설계했을 때 실제 모델의 비선형성에 의해 발생하는 제어기 성능 저하를 줄이기 위해 이득 계획 기법을 적용하였다. 시스템의 특징을 고려하여 연소관 내부 체적 변화에 따라 이득을 조절하는 방법과, 연소관 내부 압력에 의해 이득을 조절하는 방법으로 두종류의 이득 계획 제어기를 설계하였다. 각 제어기를 가변 추력기 모델에 적용하여 폐루프 시스템 응답특성을 비교하였으며 가변 추력 추진기관 특성에 따라서 어떤 제어기를 선택하는 것이 유리한지 제안하였다.

Theoretical model of a variable thrust solid rocket motor with a pintle nozzle was derived. For the chamber pressure control, classical model linearization and proportional-intergral controller was used. And then two types of gain scheduling controller were suggested to imporve controller performance for the non-linear propulsion model. Considering characteristics of systems, control gains were scheduled by chamber pressure or free volume. Step responses of each controllers were compared. As a result, the proper control algorithm about characteristics of variable thrust rocket motor was suggested.

키워드

참고문헌

  1. Bergmans, J.K. and Solvo, R., "Solid Rocket Motor Control: Theoretical Motivation and Experimental Demonstration," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, USA, AIAA 2003-4968, July 2003.
  2. Bergmans, J.L. and Myers R.I., "Throttle Valves for Air Turbo-Rocket Engine Control," AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, USA, AIAA 1997-3188, July 1997.
  3. Kim, Y.S., Cha, J.H., Ko, S.H. and Kim, D.S., "Control of Pressure and Thrust for a Variable Thrust Solid Propulsion System Using Linearization," Journal of the Korean Society of Propulsion Engineers, Vol. 15, No. 4, pp. 18-25, 2011.
  4. Joner S. and Quinquis, I., "Control of and Exoatmospheric Kill Vehicle with a Solid Propulsion Attitude Control System," AIAA Guidance, Navigation, and Control Conference and Exhibit, Keystone, CO, USA, AIAA 2006-6572, Aug. 2006.
  5. Lee, H.S., Lee, D.Y. Park, J.S. and Kim, J,K., "A Study on Pressure Control for Variable Thrust Solid Propulsion System Using Cold Gas Test Equipment," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 37, No. 1, pp. 76-81, 2009. https://doi.org/10.5139/JKSAS.2009.37.1.076
  6. Lee, W.S., Eun, Y.J., Bang H.C. and Lee, H.S., "Efficient Thrust Distribution with Adaptive Pressure Control for Multinozzle Solid Propulsion System," Journal of Propulsion and Power, Vol. 29, No. 6, pp. 1410-1419, 2013. https://doi.org/10.2514/1.B34645