The Application of an Lpv/Loop-Shaping Synthesis for a Missile Autopilot

摘要

In this paper, a gain-scheduling autopilot for a missile pitch axis is designed over a wide operating range. The parametric controller is obtained by LPV synthesis applied to the H{sub}∞ loop-shaping criterion. Robust stability and performanceare firstly checked by means of linear simulations and μ-analysis and secondly verified by using non-linear simulations, in the face of noise disturbances, aerodynamic dispersions and scheduling parameters variations.