• 대한기계학회논문집A
• /
• 제26권4호
• /
• pp.602-608
• /
• 2002

The flexible structure like solar array and antenna in spacecraft shows very sensitive responses to the inner or outer disturbance and noise. And the spacecraft becomes more complex and larger as it has various mission and role. But since the spacecraft need to have the limited mass, the thin and light material should be selected and this necessity induces the decrease d natural frequency and structural stiffness. It reduces the ability of adapting to the disturbance and induces the structural unstability. Certainly, the disturbance does not only make the structural unstability, but also give the bad effect to the precise attitude control. So it is necessary to control the vibration in the space. In this paper, the flexible structure control modeling with piezo sensor and piezo actuator is developed. The model uncertainty of damping ratio is overcome by robust control. The system equation is induced by the finite element method.

• 한국소음진동공학회논문집
• /
• 제13권10호
• /
• pp.777-784
• /
• 2003

본 논문에서는 압전소자를 이용한 코너 지지된 직사각형 박판의 음향 반응에 대한 제어에 관하여 이론과 실험적인 연구를 하였다. 3개의 각각 다른 종횡비의 알루미늄판을 사용하였고 고정은 4개의 코너에서 볼조인트를 이용하였다. 그 결과 종횡비가 가장 큰 박판에서 0∼200Hz 진동수와 80∼100dB의 음압의 가진에서 예측대로 가장 크고 선명한 응답을 보였다. 압전소자에 의한 판을 통한 음향전달 감소는 크지 않았지만, 압전소자를 이용한 음향반응 제어는 기대 이상으로 현저하였다. 본 실험은 항공기 승강문의 음장 가진에 대한 선행 연구를 확장시킨 독창적인 연구이다. 가장 중요한 차이점은 문의 조인트를 볼 조인트로 모사한 것이다.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2000년도 제15차 학술회의논문집
• /
• pp.498-498
• /
• 2000

A study on the robust control of a composite beam with a distributed PVDF sensor and piezo-ceramic actuator is presented in this paper. 1st and 2nd natural frequencies are considered in the modeling, because robust control theory which has robustness to structured uncertainty is adopted to suppress the vibration. If the controllers designed by H$_{\infty}$ theory do not satisfy control performance, it is improved by $\mu$-synthesis method with D-K iteration so that the $\mu$-controller based on the structured singular value satisfies the nominal performance and robust performance. Simulation and experiment were carried out with the designed controller and the verification of the robust control properties was presented by results.

• 한국소음진동공학회논문집
• /
• 제25권10호
• /
• pp.685-691
• /
• 2015

In this work, to identify effective parameter for performance of piezoelectric jetting dispenser, experimental investigation is carried out based on design of experiment. After preparing jetting dispenser using two stack-type piezoelectric actuators, basic working principle of the jetting dispenser is described. Eight operating conditions are chose as main factors and it is assumed that each factor has two levels. To reduce number of experiments for performance evaluation, the experimental sets are designed based on factional factorial design method. Experimental setup is established and the weight of single dot is measured by using precision scale. The main and interaction effects of factors are analyzed using commercial statistical program and optimal operating condition for small amount and small variation of weight of dispensed single dot are determined.