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This paper presents the robustified form of generalized dynamic inversion control and its application to attitude control for satellite launch vehicle. In proposed control law, dynamic constraint is prescribed in the form of asymptotically stable differential equation that encapsulate the control objectives. The constraint differential equation is evaluated along the vehicle's attitude trajectories...
This paper presents a two-loops structured control system design for quadrotor's position/attitude trajectory tracking. The aim of the outer loop is to provide the roll/pitch tilting commands to the inner loop, which in turns generates the quadrotor's tilting angles required to control the horizontal CG position. To fulfill that purpose, the outer loop utilizes Generalized Dynamic Inversion of a prescribed...
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