This program was originated for the purpose of developing a flight control system for helicopters and V/STOL vehicles. The design utilizes force stick steering and parallel servo installation with full, mechanical back-up. The system stabilizes the vehicle in all four axes with additional features such as altitude hold velocity hold, turn coordination, and attitude hold. (Author)
Integrated Pilot Assist System
1973
86 pages
Report
Keine Angabe
Englisch
Avionics , Human Factors Engineering , Aircraft , Automatic pilots , Attitude control systems , Speed regulators , Man machine systems , Integrated systems , Helicopters , Stabilization systems , Flight speeds , Vertical takeoff aircraft , Short takeoff aircraft , Observation aircraft , Servomechanisms , Feedback , Control sticks , Force(Mechanics) , Pitch(Motion) , Roll , Yaw , Simulation , Pilots , Rescues , Flight paths , Tactical warfare , Turning flight , Hovering , Altitude control systems , Fail safe design , H-6 aircraft , Strouhal number
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