A Summary of the Cassini Spacecraft Thermal Performance from Launch Through Early Cruise
A supercircular entry guidance concept designed for maximum monitoring capability
A Systematic Methodology for Modeling and Attitude Control of Multi-body Space Telescopes
A system for inertial experiment pointing and attitude control
A system for varying the stability and control of a deflected-jet fixed-wing vtol aircraft
A technique for optimal final value control of powered flight trajectories.
A TECHNIQUE FOR OPTIMUM FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES
A technique for the assessment of fighter aircraft precision controllability
A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle
A Theoretical Investigation of the Rolling Oscillations of an Airplane with Ailerons Free
A Time History of Control Operation of a C-54 Airplane in Blind Landing Approaches
Attitude control of a satellite in an elliptic orbit.
ATTITUDE CONTROL REQUIREMENTS FOR HOVERING DETERMINED THROUGH THE USE OF A PILOTED SIMULATOR
Attitude Control System and Star Tracker Performance of the Wide-Field Infrared Explorer Spacecraft
Attitude instability regions of a spinning symmetric satellite in an elliptic orbit.
Attitude stabilization using a contactor control system with a linear switching criterion.
A unique formulation of elastic airplane longitudinal equations of motion
A unique suspension system for longitudinal vibration testing of large launch vehicles
Automated Cooperative Trajectories for a More Efficient and Responsive Air Transportation System
Autonomous Guidance, Navigation, & Control (GN&C) for Next-Generation Missions
A variable structure approach to robust control of VTOL aircraft
A visual flight investigation of hovering and low-speed vtol control requirements
A wind tunnel technique for determining stability derivatives from cable mounted aeroelastic models
Behavioral Indicators in Air Traffic Control: Detecting and Preventing Performance Decline
Benchmark Active Controls Technology (BACT) Wing CFD Results
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft