AIAA-2002-4560 Generation of Launch Vehicle Abort Trajectories Using a Hybrid Optimization Method
AIAA-2002-4917 Adaptive Compensation for Flexible Dynamics
AIAA-2002-4776 A Six Degree-of-Freedom Adaptive Flight Control Architecture for Trajectory Following
AIAA-2002-4441 Flight Evaluation of Adaptive High-Bandwidth Control Methods for Unmanned Helicopters
AIAA-2002-4942 An Augmenting Adaptive Approach to Control of Flexible Systems