AIAA-2004-4870 Direct Adaptive Control for Aircraft Control Surface Failures During Gust Conditions
Eigenstructure Assignment for a Tailless Aircraft AIAA Paper
Simple Adaptive Control in the Delta Domain using a Linear Matrix Inequality (AIAA 2014-0085)
Reconfigurable Delta Operator Eigenstructure Assignment for a Tailless Aircraft
Robust Multirate Eigenstructure Assignment with Flight Control Application
Simple Adaptive Control for Aircraft Control Surface Failures