Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations
Application of frequency-domain handling qualities criteria to the longitudinal landing task
Application of leading-edge vortex manipulations to reduce wing rock amplitudes
Application of parameter estimation to highly unstable aircraft
Application of precomputed control laws in a reconfigurable aircraft flight control system
Application of the equilibrium spin technique to a typical low-wing general aviation design
Application of the pitch modulation maneuver in the region of the ''limiting'' entry velocity.
Application of transonic codes to aeroelastic modeling of airfoils including active controls
Appreciation and prediction of flying qualities
Approach for Structurally Clearing an Adaptive Compliant Trailing Edge Flap for Flight
Approach trajectory guidance for maximum concealment
A Presentation on Robust Flutter Margin Analysis and a Flutterometer
A program for optimal design of distributed microcomputer flight control and navigation structures
Areas of research on surfaces for thermal control
A Remote Vehicle Operations Center’s Role in Collecting Human Factors Data
A review of helicopter control-display requirements for decelarating instrument approach
A Review of System Identification Methods Applied to Aircraft
A Robust Control Approach for the Formation Flying of Multiple Spacecraft
A robust direct-integration method for rotorcraft maneuver and periodic response
A Robust Uniform Control Approach for VTOL Aircraft
Artificial Immune System Approach for Airborne Vehicle Maneuvering
Ascent, Transition, Entry, and Abort Guidance Algorithm Design for the X-33 Vehicle
A SIMPLE SOLAR ORIENTATION CONTROL SYSTEM FOR SPACE VEHICLES
A simulation study of curved, descending, decelerating, landing approaches for transport aircraft
A Small Spacecraft Swarm Deployment and Stationkeeping Strategy for Sun-Earth L1 Halo Orbits
A split-damper inertially coupled passive gravity-gradient attitude control system.
Assessment of Remote Pilot Maneuver Taskload under Multi-Vehicle Control
A status report on NASA general aviation stall/spin flight testing
A STUDY OF A PILOT'S ABILITY TO CONTROL DURING SIMULATED STABILITY AUGMENTATION SYSTEM FAILURES
A study of stall deterrent systems for general aviation aircraft
A study of the effect of adverse yawing moment on lateral maneuverability at a high lift coefficient
A study to determine the characteristic shapes of helicopter visual approach profiles
A Summary of the Cassini Spacecraft Thermal Performance from Launch through Early Cruise
A Summary of the Cassini Spacecraft Thermal Performance from Launch through Early Cruise