A computer study was made of the lateral response of a T-33 aircraft cruising at 450 mph true air speed at 35000 feet with tip tanks empty using a Summers 1025A Pilot Assist System. Studies of required gains and tilt angle were conducted. (Author)
Computer Study of the Lateral Response of a T-33 Aircraft Using a Simulated Summers 1025A Pilot Assist System
1954
52 pages
Report
No indication
English
Navigation, Guidance, & Control , Structural Mechanics , Aircraft , Jet training planes , Automatic pilots , Aerodynamic characteristics , Programming(Computers) , Yaw , Roll , Test methods , Gyroscopes , Sensitivity , Mathematical models , T-33 aircraft , Rate gyroscopes , Computerized simulation , Computer analysis
Study of characteristics of human-pilot control response to simulated aircraft lateral motions
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