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Stabilität
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keywords:(Stabilität)
Improvement of helicopter attitude stability by active control of the conventional swash plate
Aeroelastic stability and response of rotating structures
Determination of the stability and control derivatives of the NASA F/A-18 HARV using flight data
ACSYNT inner loop flight control design study
Fidelity assessment of a UH-60A simulation on the NASA Ames vertical motion simulator
Aerodynamic flight control to increase payload capability of future launch vehicles
Research in robust control for hypersonic aircraft
Criteria for design of integrated flight/propulsion control systems for STOVL fighter aircraft
Simulator evaluation of displays for a revised takeoff performance monitoring system
High-speed civil transport flight- and propulsion-control technological issues
Assessment of flying-quality criteria for air-breathing aerospacecraft
Control integration concept for hypersonic cruise-turn maneuvers
NASA TSRV essential flight control system requirements via object oriented analysis
Design and analysis issues of integrated control systems for high-speed civil transports
Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data
Thrust vectoring for lateral-directional stability
Design and experimental validation of a flutter suppression controller for the active flexible wing
Research in robust control for hypersonic vehicles
Modeling and model simplification of aeroelastic vehicles: An overview
Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics
A feasibility study regarding the addition of a fifth control to a rotorcraft in-flight simulator
Aeroservoelastic stabilization techniques for hypersonic flight vehicles
Trim drag reduction concepts for horizontal takeoff single-stage-to-Orbit vehicles
Application of nonlinear feedback control theory to supermaneuverable aircraft
Rapid near-optimal aerospace plane trajectory generation and guidance
Initial piloted simulation study of geared flap control for tilt-wing V/STOL aircraft
The integrated manual and automatic control of complex flight systems
The integrated manual and automatic control of complex flight systems
The integrated manual and automatic control of complex flight systems
The integrated manual and automatic control of complex flight systems
Controlling crippled aircraft-with throttles
Modeling, simulation, and flight characteristics of an aircraft designed to fly at 100,000 feet
Guidance and control strategies for aerospace vehicles
Aerodynamic parameters of High-Angle-of attack Research Vehicle (HARV) estimated from flight data
Fly-by-light flight control system technology development plan
Crew emergency return vehicle autoland feasibility study