LQG/LTR CONTROLLER DESIGN FOR AN AIRCRAFT MODEL

Abstract

The automation of the operation of aircraft equipment lightens and diminishes the manipulation of the pilot during the flight. This article gives some introduction about the fundamental aspects of the LQG/LTR control theory, and it shows an application option through an example. The movement of an aircraft can be modeled with a linear time invariant dynamic system, which must be controlled by a flight controller. This article contains the synthesis and analysis of the stability and other qualitative control parameters of the flight control.