Guaranteed cost control of stochastic uncertain systems applied to a problem of missile autopilot design
Abstract
In this paper, we apply a recent result on output feedback guaranteed cost control of stochastic uncertain systems to the problem of designing a missile autopilot. In the missile autopilot design problem, the given data is a finite collection of plant models for the missile corresponding to different flight conditions. A total least squares approach is used to fit the data to a norm bounded uncertain system model.