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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格式: | Research Report |
語言: | English |
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2008
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在線閱讀: | http://hdl.handle.net/10356/14251 |
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