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Standsicherheit
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Guidance and control strategies for aerospace vehicles
Guidance and control strategies for aerospace vehicles
NASA B737 flight test results of the total energy control system
Simulation evaluation of two VTOL control/display systems in IMC approach and shipboard landing
Flight tests of the Digital Integrated Automatic Landing System (DIALS)
Flutter prediction for a wing with active aileron control
Helicopter simulation validation using flight data
Configuration management and automatic control of an augmentor wing aircraft with vectored thrust
Effects of relaxed static longitudinal stability on a single-stage-to-orbit vehicle design
Important factors in the maximum likelihood analysis of flight test maneuvers
Modal control theory and application to aircraft lateral handling qualities design
SCAR arrow-wing active flutter suppression system
The design of digital-adaptive controllers for VTOL aircraft
Application of active controls technology to aircraft bide smoothing systems
Stability and control derivatives of the T-37B airplane
Investigation of the Multiple Model Adaptive Control (MMAC) method for flight control systems
HARV ANSER Flight Test Data Retrieval and Processing Procedures
Application of Wind Tunnel Free-Flight Technique for Wake Vortex Encounters
An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities
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
Experience with synchronous and asynchronous digital control systems
Prediction of wing aeroelastic effects on aircraft lift and pitching moment characteristics