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An electronic control for an electrohydraulic active control landing gear for the f-4 aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ross, I. |
| Copyright Year | 1982 |
| Description | 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%. |
| File Size | 4428662 |
| Page Count | 95 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820014378 |
| Archival Resource Key | ark:/13960/t71w0bj1s |
| Language | English |
| Publisher Date | 1982-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Potential Energy Craters Rolling Contact Loads Landing Loads Hydraulic Control Landing Gear Servocontrol F-4 Aircraft Kinetic Energy Active Control Computer Aided Design Aircraft Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
