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Description of the Spacecraft Control Laboratory Experiment (SCOLE) facility
A survey of handling qualities criteria and their applications to high performance aircraft
Mission-oriented requirements for updating MIL-H-8501. Volume 1: STI proposed structure
Development of ADOCS controllers and control laws. Volume 1: Executive summary
Flying qualities and control system characteristics for superaugmented aircraft
Main rotor six degree-of-freedom isolation system analysis
Terminal area automatic navigation, guidance, and control 1: Automatic rollout, turnoff, and taxis
Active flutter control for flexible vehicles, volume 1
Simulation study of the oscillatory longitudinal motion of an airplane at the stall
Lightning effects on the NASA F-8 digital-fly-by-wire airplane
Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane
The X-31A quasi-tailless flight test results
High-Alpha Handling Qualities Flight Research on the NASA F/A-18 High Alpha Research Vehicle
Fuzzy Logic Decoupled Longitudinal Control for General Aviation Airplanes
Icing effects on aircraft stability and control determined from flight data: Preliminary results
Application of nonlinear feedback control theory to supermaneuverable aircraft
Guidance and control strategies for aerospace vehicles
National remote computational flight research facility
Multiplexing electro-optic architectures for advanced aircraft integrated flight control systems
Development and demonstration of an on-board mission planner for helicopters
Helicopter roll control effectiveness criteria program summary
Development and flight test experiences with a flight-crucial digital control system
Validation of a real-time engineering simulation of the UH-60A helicopter
Aeroelastic control of oblique-wing aircraft
Experience with synchronous and asynchronous digital control systems
Prediction of wing aeroelastic effects on aircraft lift and pitching moment characteristics
Space shuttle flying qualities criteria assessment, phase 3
V/STOLAND avionics system flight-test data on a UH-1H helicopter
Hybrid LTA vehicle controllability as affected by buoyancy ratio