๐”– Bobbio Scriptorium
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FAULT TOLERANT CONTROL SYSTEM: QFT DESIGN

โœ Scribed by M. S. Keating; M. Pachter; C. H. Houpis


Publisher
John Wiley and Sons
Year
1997
Tongue
English
Weight
554 KB
Volume
7
Category
Article
ISSN
1049-8923

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โœฆ Synopsis


This paper addresses flight control system synthesis and the accommodation of controlled plant variation in an aircraft design envelope by using the frequency domain based quantitative feedback theory (QFT) robust control system design method. Plant variations considered include varying flight conditions in the flight envelope and damage to aerodynamic control surfaces. A robust flight control system is designed for the aircraft's longitudinal and lateral directional channels and validated with simulations containing nonlinear saturation elements.


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