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By ALPER AKMEŞE

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Additional resources for AEROSERVOELASTIC ANALYSIS AND ROBUST CONTROLLER SYNTHESIS FOR FLUTTER SUPPRESSION OF AIR VEHICLE CONTROL ACTUATION SYSTEMS

Sample text

How far could it bend? If the people who asked these questions are alive, the answer of the first question is yes. The answer of the second question is in the field of aeroelasticity. ”Aeroelasticity is the study of the effect of aerodynamic forces on elastic bodies” [1]. In Figure 1, the aeroelastic triangle of forces introduced by Collar is given [ 2 ]. This figure also describes the classification of aeroelasticity problems. In Figure 1, A, E, and I represent the Aerodynamic, Elastic, and Inertial forces, respectively.

30], and Laurenson et al. [31], controller synthesis for control actuation systems of fully movable elastic control surfaces was rare. While H∞ and µ are robust controller methods, H2 is basically a LQG/LQR controller using similar definitions with robust controller methods for the construction of the synthesis problem. Controllers synthesized by means of these three methods have different advantages over each other. The H2 controller stands out with current consumption performance and tracking performance at the design conditions.

13) Roger’s method has the advantage of defining different number of aerodynamic lag terms for each modal aerodynamic force coefficient. With this property, Roger’s method can define the aerodynamic forces with the best approximation among the four rational function approximation methods. 14) for rational function approximation. 14), were assigned for each term of modal aerodynamic force coefficient matrix. This assignment reduces the order of the equations of motion. On the other hand, it also reduces the success of the rational function approximation.

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