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Space shuttle flying qualities and criteria assessment
Autonomous flight and remote site landing guidance research for helicopters
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
An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities
Flight-Determined Stability and Control Characteristics of the M2-F3 Lifting Body Vehicle
The Case for Inherent Stability of Helicopters
Investigation of piloting aids for manual control of hypersonic maneuvers
Criteria for design of integrated flight/propulsion control systems for STOVL fighter aircraft
Design and experimental validation of a flutter suppression controller for the active flexible wing
Research in robust control for hypersonic vehicles
Digital control of highly augmented combat rotorcraft
Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
Flared landing approach flying qualities. Volume 2: Appendices
Highly Maneuverable Aircraft Technology (HiMAT) flight-flutter test program
Enhanced manual controllability via active control of aeroelastic vehicles
Quiet Short-Haul Research Airplane (QSRA) model select panel functional description
Dynamic structural aeroelastic stability testing of the XV-15 tilt rotor research aircraft
Application of variable structure system theory to aircraft flight control
Effect of a flexibly mounted store on the flutter speed of a wing
An analytical study of effects on aeroelasticity on control effectiveness