Design of reliable and reconfigurable auto-landing flight controller

Design of reliable and reconfigurable auto-landing flight controller

Part I of this report presents the methodology of reliable autolanding control design for aircraft. The nonlinear aircraft model is first linearized at various flight conditions under various fault conditions that covers the entire flight regime intended and all fault scenarios. Then a linear air...

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Bibliographic Details
Main Authors: Wang, Jianliang, Narasimhan Sundararajan
Other Authors: School of Electrical and Electronic Engineering
Format: Research Report
Language:English
Published: 2008
Subjects:
DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
Online Access:http://hdl.handle.net/10356/14251

Internet

http://hdl.handle.net/10356/14251

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