The report describes six different research and development activities in flight control actuation. The activities are: (1) the development and test of a unique linear actuator sealing system for high-pressure systems, (2) the development and test of a digital servovalve using piezo-controlled high-speed solenoid valves, (3) the performance evaluation of an F-15 rudder actuator under applied loads, (4) the performance evaluation of a Mission Adaptive Wing section under different load conditions, (5) the evaluation of output impedance modification of an electrohydraulic actuator for flutter suppression, and (6) the development and test of a direct drive valve and electronics (analog and digital) for an F-16 Horizontal Tail/FlapeRon actuator. This volume presents activities 1.2. and 3. Volume II presents activities 4. 5. and 6. (KR)
Advanced Actuation Systems Development. Volume 1
1989
233 pages
Report
No indication
English
Avionics , Aircraft , Actuators , Flight control systems , Adaptive systems , Digital systems , Drives , Electronics , Flutter , High pressure , Impedance , Linear systems , Loads(Forces) , Missions , Modification , Output , Performance tests , Sealed systems , Servovalves , Suppression , Wings
Advanced Actuation Systems Development. Volume 2
NTIS | 1989
|British Library Online Contents | 1998
|Online Contents | 1998
|Emerald Group Publishing | 1998
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