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AIAA Guidance, Navigation, and Control Conference
This paper presents a loop shaping LPV controller for the NASA-HL-20 atmospheric reentry vehicle model provided by DEIMOS Space (Spain). The control problem consists of tracking a reference approach trajectory by appropriately controlling the longitudinal motion of the vehicle. The controller is designed using the tools developed at the University of Leicester within phase I of the collaborative LPVMAD project funded by the European Space Agency (LPV Gain Scheduling Techniques for Spacedoi:10.2514/6.2009-5635 fatcat:kdahvec6lbhnldg5r74elvgj4i