Abstract
This paper develops a robust H∞ controller for a pitching and plunging airfoil using the state space representation of Theodorsen's lift model employing the linear matrix inequalities (LMI) method. Both parameter uncertainty and the input disturbances are considered in the model. The existence condition for the robust H∞ state-feedback controller is obtained using the Lyapunov functional approach. In practical systems, it is difficult to obtain all the states of the model needed for the controller. Thus the observer existence condition is proposed to provide the states' information for the model. Several examples are used to demonstrate the effectiveness of the designed controller and the designed observer.
Original language | English |
---|---|
DOIs | |
State | Published - 2013 |
Event | 31st AIAA Applied Aerodynamics Conference - San Diego, CA, United States Duration: Jun 24 2013 → Jun 27 2013 |
Conference
Conference | 31st AIAA Applied Aerodynamics Conference |
---|---|
Country/Territory | United States |
City | San Diego, CA |
Period | 06/24/13 → 06/27/13 |