Journal of the Korean Society of Propulsion Engineers (한국추진공학회지)

The Korean Society of Propulsion Engineers (한국추진공학회)
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Research for Thrust Distribution Method of DACS for Response to Pintle Actuating Failure

DACS 추진기관의 핀틀 구동장치 고장을 허용하는 추력 분배기법 연구

  • Ki, Taeseok (The 4th R&D Institute - 5th Directorate, Agency for Defense Development)
  • Received : 2016.12.27
  • Accepted : 2017.07.03
  • Published : 2017.10.01
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Abstract

Robust thrust distribution method of solid DACS is researched. For the case of the system which has higher number of actuation nozzles than the degree of freedom of thrust to be controlled, the robust thrust allocation law which accommodate the abnormal operation is suggested. Assuming the situation that some nozzles are uncontrollable, the error between nozzle throat area command and response can be calculated. The error is used for realtime reshaping of weighting matrix. From the weighting effect, the nozzle which operated abnormally has low responsibility for the command then, the thrust error is reduced. The suggested algorithm is verified by the simulation of abnormal operation condition of DCS and ACS nozzle respectively.

고체 추진제를 연료로 사용하는 DACS의 강인한 추력 분배기법에 대한 연구를 수행하였다. 추진기관이 제어해야 하는 추력의 자유도보다 많은 구동 노즐을 보유한 시스템에 대하여, 비정상적인 상황을 허용할 수 있는 강인한 추력제어 기법을 제안하였다. 추력 분배기법에 의해 각 노즐로 인가된 명령 대비 응답 노즐 목 면적 크기의 차이를 이용하여 추력 분배기법에 적용된 가중행렬을 실시간으로 변환시키는 기법을 적용하였다. 이를 통하여 오차가 발생한 노즐의 추력 분배 비율을 감소시키고, 결론적으로 시스템에서 발생되는 추력 오차를 감소시키도록 하였다. 제안된 기법에 대하여 DCS와 ACS 각각의 구동장치가 제어명령을 추종하지 못하는 임의의 고장조건을 모의하였고, 시뮬레이션을 통해 기법의 성능을 검증하였다.

Keywords

References

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