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In this paper, an applicative example of multi-objective control based on linear matrix inequalities (LMIs) is presented. A dynamic output feedback attitude controller is designed for flexible satellites subject to persistent disturbance model uncertainty and the actuator saturation. The controller is assumed to have an observer-based structure and the non-linearity due to saturation is incorporated...
An integrated modeling and control strategy of payloads platform and flight control system (FCS) is presented for high altitude long endurance unmanned aerial vehicle (HALE UAV). Different from the traditional control method that UAV and payloads platform are modeled and controlled separately, an integrated control idea considering both payloads platform and FCS as a whole is proposed. First, integrated...
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