Theis, JulianJulianTheisPfifer, HaraldHaraldPfiferKnobloch, AndreasAndreasKnoblochSaupe, FlorianFlorianSaupeWerner, HerbertHerbertWerner2020-09-252020-09-252015-01AIAA Guidance, Navigation, and Control Conference (2015-01)http://hdl.handle.net/11420/7398The feedforward path of an autopilot is designed for the longitudinal dynamics of a tacti- cal missile. A linear parameter-varying model is used to synthesize a self-scheduled control law based on a parameter-dependent Lyapunov function. The controller is evaluated on a nonlinear model of industrial complexity both under nominal conditions and parametric uncertainty. Tracking performance is significantly enhanced while leaving robustness properties of an existing feedback controller unaltered.enConference PaperOther