Design of reliable and reconfigurable auto-landing flight controller

• المؤلفون الرئيسيون: Wang, Jianliang, Narasimhan Sundararajan
• مؤلفون آخرون: School of Electrical and Electronic Engineering
• التنسيق: Research Report
• اللغة: English
• منشور في: 2008
• الموضوعات: DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/14251

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...