By ALPER AKMEŞE
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Extra resources for AEROSERVOELASTIC ANALYSIS AND ROBUST CONTROLLER SYNTHESIS FOR FLUTTER SUPPRESSION OF AIR VEHICLE CONTROL ACTUATION SYSTEMS
32], Tang et al. [33, 34], Lee et al. , Price et al. , Brase et al. , and Yıldız  performed a flutter analysis of airplane wings or missile fins with several types of structural nonlinearities. In addition to the nonlinearities studied in literature, it is known by experience through the studies performed in TÜBİTAK-SAGE that the backlash type nonlinearity usually exists in the missile fins. In line with the research needs of TÜBİTAK-SAGE, aeroservoelastic analysis and controller synthesis for flutter suppression of missile control surfaces are defined as the research subject of this study with the following primary objectives.
16 In Chapter 4, controller synthesis methods for the flutter suppression are given. The aeroservoelastic model of the fin is constructed by using the aeroelastic model defined in Chapter 2. The µ flutter search method is implemented on this model. The proposed controller synthesis method for flutter suppression is presented. In order to compare the performance of this method, an alternative method is given. S.  which was originally applied to an airplane wing model. In Chapter 5, the analysis tools that are developed for the purpose of performance and LCO analyses of the aeroservoelastic system are presented.
Fokker Company stated that the prototype wing showed no structural deficiencies. The only difference between the prototype wings and the production wing was the strengthening of the rear spar. This was ordered by the Luftwaffe, due to regulations for wire braced wings. Ironically, strengthening the rear spars moved the elastic axis backwards which resulted in a decrease of the divergence speed, which eventually caused the loss of Fokker D-8 aircrafts. After WW1 many flutter phenomena were seen; in 1923 wingaileron flutter was seen in von Berkel Seaplane (monoplane), which was solved by Baumhauer and Koning by mass-balancing the aileron.