Options
Linear parameter-varying feedforward control: A missile autopilot design
Publikationstyp
Conference Paper
Date Issued
2015-01
Sprache
English
Institut
TORE-URI
Citation
AIAA Guidance, Navigation, and Control Conference (2015-01)
Contribution to Conference
Scopus ID
The 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.