한국항공우주학회지 (Journal of the Korean Society for Aeronautical & Space Sciences)

  • 제48권6호
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  • Pages.431-441
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  • 2020
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  • 1225-1348(pISSN)
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  • 2287-6871(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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오버슈트 탐지 로직 및 피드포워드 외란관측기를 활용한 제어 성능 개선 연구

Control Performance Improvement Using Overshoot Detecting Logic and Feedforward Disturbance Observer

  • 투고 : 2020.02.21
  • 심사 : 2020.05.20
  • 발행 : 2020.06.01
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초록

이 논문에서 제안된 새로운 제어 기법은 외부 외란 및 모델 불확실성으로 인해 발생하는 오버슈트를 줄여주어 제어기의 안정성 및 강건성을 보장하기 위하여 제안되었다. 제안된 제어 기법은 외란 관측기와 피드포워드 제어기, 그리고 오버슈트 탐지기로 구성되며, 간단한 구조로 구성되어 있으므로 제어 이득 설계가 용이한 장점이 있다. 이를 보이기 위해서 F-16 비행체의 종축 모델을 대상으로 시뮬레이션을 수행하였다. 또한 3가지 형태의 불확실성 모델을 반영해봄으로써 제어 성능 및 안정성을 보장할 수 있음을 확인하였으며, 루트 로커스 선도와 보드 선도를 이용하여 제안된 기법의 강인성 및 안정성을 검증하였다.

In this paper, we propose a new method using a feedforward disturbance observer that guarantees stability and robustness about the effects of external disturbance and model uncertainty. The method is consist of a disturbance observer, a feedforward controller, and an overshoot detecting logic. It has an advantage of reducing the excessive overshoot by external disturbance and model uncertainty. Also, it is easy to adjust the control gain due to a simple structure. In order to verify the effectiveness of a new method, simulation results are given for longitudinal model of F-16 aircraft. By reflecting a various of model uncertainties, the stability and the robustness are guaranteed. Finally, the stability and the robustness of the proposed method are verified using root locus plot and bode plot.

키워드

참고문헌

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