Blending Methodology of Linear Parameter Varying Control Synthesis of F-16 Aircraft System
FULL-LENGTH PAPERS - Worst-Case Analysis of the X-38 Crew Return Vehicle Flight Control System
Closed Loop Control Law Stability and Performance Analysis Directly Using Open Loop Flight Test Data
Robustness Analysis on Pitch Control Law for an Executive Transport Aircraft
Worst Case Analysis of the Flight Control System X-38 Crew Rerum Vehicle
An LMI-Based Analysis for Adaptive Flight Control with Unmodeled Input Dynamics