Homing missile guidance law with imperfect measurements and imperfect information about the system

TL;DR

This paper develops a guidance law for homing missiles considering imperfect measurements and incomplete system information, providing a more realistic model for missile guidance under practical conditions.

Contribution

It introduces a generic model of imperfect missile dynamics along with a guidance law that accounts for measurement and information imperfections.

Findings

Guidance law improves robustness under measurement errors

Model captures real-world missile dynamics more accurately

Enhances missile guidance performance in uncertain environments

Abstract

In this study, the generic imperfect dynamic models of air-to-surface missiles are given in addition to the related simple guidance law.