APPLICATION OF LIMIT-CYCLE AND PARAMETERPERTURBATION ADAPTIVE TECHNIQUES TO CONTROL OF THE FLEXIBLE SUPERSONIC TRANSPORT.
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OHIO
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The parameter-perturbation study stresses the design of a suitable gain changer, while the limit-cycle study stresses controller design. Areas of investigation include the effects of elasticity and sensor blending techniques the design of a low-frequency limit-cycle system a parameter-perturbation adaptive control system and a normal-acceleration control system.