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Frequency domain approach to guidance system design

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1 Author(s)
Rafael Yanushevsky ; Res. & Technol. Consulting, Bethesda

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.

Published in:

IEEE Transactions on Aerospace and Electronic Systems  (Volume:43 ,  Issue: 4 )