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
Keine Angabe
Englisch
Mathematical models , Aerodynamic characteristics , Computerized simulation , Aircraft , T-33 aircraft , Structural Mechanics , Sensitivity , Automatic pilots , Rate gyroscopes , Jet training planes , Computer analysis , Navigation, Guidance, & Control , Programming(Computers) , Test methods , Gyroscopes , Roll , Yaw
Study of characteristics of human-pilot control response to simulated aircraft lateral motions
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