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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書目詳細資料
Main Authors: Wang, Jianliang, Narasimhan Sundararajan
其他作者: School of Electrical and Electronic Engineering
格式: Research Report
語言:English
出版: 2008
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在線閱讀:http://hdl.handle.net/10356/14251
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