A controller for an electrohydraulic active control landing gear was developed for the F-4 aircraft. A controller was modified for this application. Simulation results indicate that during landing and rollout over repaired bomb craters the active gear effects a force reduction, relative to the passive gear, or approximately 70%.
An electronic control for an electrohydraulic active control landing gear for the F-4 aircraft
1982-04-01
Report
No indication
English
Fuzzy Control of Aircraft Semi-active Landing Gear System
British Library Conference Proceedings | 1999
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