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X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-31A System Identification Applied to Post-Stall Flight: Aerodynamics and Thrust Vectoring
X-31A High Angle of Attack and Initial Post Stall Flight Testing
Vstol Aircraft Stability and Control Experience from Methods and Results of Do 31 Flight Tests
Vista/F-16 Multi-Axis Thrust Vectoring (MATV) Control Law Design and Evaluation
Verification and Tuning of an Adaptive Controller for an Unmanned Air Vehicle
Utilization of Simulation to Support F-14A Low Altitude High Angle of Attack Flight Testing
Using Engine Thrust for Emergency Flight Control: MD-11 and B-747 Results
USCGC HEALY (WAGB 20) Results of Performance and Special Trials
UH-60A Black Hawk Engineering Simulation Program. Volume 1: Mathematical Model
Trail Maneuver Generation and Selection in the Paladin Tactical Decision Generation System