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Timely Actions Needed to Advance the Next Generation Air Transportation System
Time Domain Analysis of a Rigid Two-Bladed Fully Gimballed Helicopter Rotor with Circulation Control
Tightly Coupled GPS-Gyro Integration for Spacecraft Attitude Determination
Thrust Vectoring Control System for Rocket Nozzles
Thrust Vectoring Apparatus for Maneuvering Missile in Flight
Thrust Vector Control System Study for a Large Liquid Booster
Thrust Vector Controland Visualisation for Stovl Aircraft
Thrust Vector Aided Maneuvering of the YF-22 Advanced Tactical Fighter Prototype
Three-Cue Helicopter Flight Director Evaluation
Three-Axis Fluidic/Electronic Automatic Flight Control System Flight Test Report
Three-Axis Dynamic Simulation of Helicopter Angular Motion for Testing Fire Control Materiel
Third Annual Workshop on Space Operations Automation and Robotics (Soar 1989)
The Wake Steering Nozzle: A New Method of Steering Submersibles
The Use of Piloted Flight Simulators in General Research
The Technical Equipment of Computerized Control Systems (Selected Pages)
Thermodynamic and Ballistic Design Fundamentals of Solid-Propellant Rocket Engines
Thermal Margins for Flight Electronics Review and Assessment
Thermally Actuated Valves Final Report, 15 Dec. 1969 - 15 Jul. 1970
Thermal considerations for electronics packaging of the Nimbus spacecraft control system.
The reliability contribution of the pilot to a large launch vehicle control system.
The Performance of a Conceptual Vertical Attitude Takeoff and Landing Fighter Aircraft
Theory of Remote-Control and Homing Guidance Systems of Rockets
Theory of Helicopter Damping in Pitch or Roll and a Comparison With Flight Measurements
Theory of Control of the Motion of Spacecraft (Selected Chapters)
Theory and Design of Adaptive Automation in Aviation Systems
The Operational Effects of Automatic Ramp Control on Network Traffic