Title :
Frequency domain approach to guidance system design
Author :
Yanushevsky, Rafael
Author_Institution :
Res. & Technol. Consulting, Bethesda
fDate :
10/1/2007 12:00:00 AM
Abstract :
The frequency domain approach to guidance system design is presented. The model of the guidance control system reflects the most important characteristics of the flight control system that combines airframe and autopilot dynamics (damping, natural frequency, time constant, and airframe zero frequency). The analytical expressions for frequency response and related expressions for missile system performance are given. The analytical results obtained can be utilized for missile system design.
Keywords :
aircraft control; aircraft navigation; frequency response; frequency-domain analysis; missile guidance; airframe zero frequency; autopilot dynamics; flight control system characteristics; frequency domain approach; frequency response; guidance control system design; missile system design; missile system performance; proportional navigation guidance system; Acceleration; Aerospace control; Control theory; Damping; Frequency domain analysis; Frequency response; Missiles; Navigation; Performance analysis; System performance;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2007.4441757
