Loading...
Please wait, while we are loading the content...
Similar Documents
Redundant actuator development program. [for flight control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fain, D. M. Svensson, C. I. Chenoweth, C. C. |
| Copyright Year | 1975 |
| Description | Two concepts of redundant secondary actuator mechanization, applicable to future advanced flight control systems, were studied to quantitatively assess their design applicability to an AST. The two actuator concepts, a four-channel, force summed system and a three-channel, active/standby system have been developed and evaluated through analysis, analog computer simulation, and piloted motion simulation. The quantitative comparison of the two concepts indicates that the force summed concept better meet performance requirements, although the active/standby is superior in other respects. Both concepts are viable candidates for advanced control application dependent on the specific performance requirements. |
| File Size | 4275477 |
| Page Count | 166 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750013217 |
| Archival Resource Key | ark:/13960/t3pw18g36 |
| Language | English |
| Publisher Date | 1975-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Actuators Redundancy Systems Engineering Reliability Engineering Aircraft Design Flight Control Aircraft Configurations 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 |
