A Simple Linear Design Methodology for Two Loop Lateral Missile Autopilot

摘要

A methodology for linear design of two-loop lateral missile autopilot has been proposed in this paper. The design approach enables to obtain admissible control gains satisfying the stability margin specifications, from a simple set of parametric equations involving the missile system. The parametric equations developed help in assessing the significance of each parameter on system performance. The step-by-step design methodology for the proposed algorithm has been given in details and illustrated with numerical examples using four different types of missile data.