Abstract:Dynamic modeling and control of two-degree-of-freedom launchers which are utilized for launching munitions such as missiles and rockets have become one of the most popular fields in recent years. Control of launch vehicles gains more importance especially when they are mounted on moving vehicles. In this study, the mathematical modeling and control with parameter uncertainties of a high-accuracy two-degree-of-freedom electromechanically-actuated launcher are investigated in the direction of reducing the impact… Show more
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