Robust Aeroservoelastic Control Utilizing Physics-Based Aerodynamic Sensing

摘要

The paper describes the design of aeroservoelastic controllers using H_∞ and LPV control design techniques for a Body Freedom Flutter aircraft. The controllers are compared in the frequency and time domain The LPV controller does not achieve the level of performance of the individual H_∞ controllers, though the performance achieves the desired objectives. The similarities and difference between the designs are discussed.