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Stabilität
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Quasi-steady flight to quasi-steady flight transition in a windshear - Trajectory guidance
Aircrew-aircraft integration: A summary of US Army research programs and plans
An integrated development of the equations of motion for elastic hypersonic flight vehicles
Assessment of proposed fighter agility metrics
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
Interactive flutter analysis and parametric study for conceptual wing design
Concepts for pilot interaction with an automated NOE obstacle-avoidance system
Hypersonic vehicle control law development using H infinity and mu-synthesis
Hypersonic vehicle control law development using H infinity and mu-synthesis
Modeling, model simplification and stability robustness with aeroelastic vehicles
Rotary-wing aeroelasticity with application to VTOL vehicles