Session Track
April 26 (Friday)
항공우주 부품개발Ⅰ
Oral,
제 3 발표장(로즈룸)
- 김재원
FA3-1
A semi active control for a full aircraft landing gear model
Semi active landing gear can provide good performance in difference landing scenarios. Particularly, semi active landing gear using magnetorheological damper is the most candidate to replace the passive damper. In this paper, the full aircraft landing gear model with three points landing gear case is build using SIMSCAPE (MATLAB). To reduce the acceleration of aircraft, semi active control methods are developed and compare. In this paper, sliding mode control, and optimal control are applied to compare with passive damper. The result of numerical simulation shows that the acceleration of aircraft can be significantly reduced by using optimal control compared to other control algorithms.
Keywords :
Landing Gear, SIMSCAPE – Simulink, Semi Active Control, Full Aircraft Model, optimal control, sliding mode control
Paper : FA3-1.pdf
항공우주시스템공학회, 대전광역시 중구 계백로 1719(오류동, 센트리오피스텔 제 12층 1206호)
Tel: 042-523-1978, E-mail: sase@sase.or.kr