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Automatic Control of Aircraft

  • Ashish Tewari
Chapter
Part of the Control Engineering book series (CONTRENGIN)

Abstract

To derive linear aircraft flight dynamics plant for use in automatic flight control system design. To decouple aircraft dynamics into longitudinal and lateral-directional plants, and to briefly study the stability and control derivatives. To consider modeling of servo actuators for aircraft’s engine and control surfaces. To present single- and multi-variable automatic flight control systems (stability augmentation systems and autopilots) for both longitudinal and lateral-directional dynamics. To design and analyze aircraft control systems using both transfer function and state-space methods

Keywords

Fatigue Vortex Torque Radar Compressibility 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Copyright information

© Springer Science+Business Media, LLC 2011

Authors and Affiliations

  1. 1.Department of Aerospace EngineeringIndian Institute of TechnologyKanpurIndia

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