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Flight investigation of variations in rotorcraft control and display dynamics for hover
Description of the Spacecraft Control Laboratory Experiment (SCOLE) facility
Design of a candidate flutter suppression control law for DAST ARW-2
Rotary-wing aeroelasticity with application to VTOL vehicles
Model order reduction applied to a hot-bench simulation of an aeroelastic wind-tunnel model
Subsonic pitch-up alleviation on a 74 deg delta wing
Preliminary assessment of the robustness of dynamic inversion based flight control laws
Yaw rate control of an air bearing vehicle
Impact of flying qualities on mission effectiveness for helicopter air combat, volume 1
Interactive flutter analysis and parametric study for conceptual wing design
Automatic guidance and control laws for helicopter obstacle avoidance
Self-tuning Generalized Predictive Control applied to terrain following flight
A review of US Army aircrew-aircraft integration research programs