The feasibility of the Advanced Flight Control Actuation System (AFCAS) concept was demonstrated in a T-2C aircraft. The test installation contained a localized 8000 psi (55 MPa) hydraulic power supply, control-by-wire direct-drive modular design rudder actuator, electronic drive unit, and force transducer. The system performed exceptionally well during 10.2 hours of flight evaluation. Successful completion of this project confirmed prior analyses and laboratory testing. (Author)
Flight Verification of the Advanced Flight Control Actuation System (AFCAS) in the T-2C Aircraft
1978
149 pages
Report
Keine Angabe
Englisch
Aircraft flight control actuation system design
TIBKAT | 1993
|Flight Control Actuation - All Electric Aircraft
British Library Conference Proceedings | 1993
|