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An analytical study of airplane-autopilot response to atmospheric turbulence
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Oehman, W. I. |
| Copyright Year | 1972 |
| Description | An analytical study has shown that, with proper selection of feedback gains, an automatic control system can reduce excursions in altitude of a jet transport flying in turbulence without increasing structural loads. The control system uses feedback of attitude-angle and pitch-rate signals to the elevator and uses feedback of altitude and altitude-rate signals to the throttle. |
| File Size | 1315875 |
| Page Count | 45 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720022359 |
| Archival Resource Key | ark:/13960/t8bg7fm6x |
| Language | English |
| Publisher Date | 1972-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Equipment Specifications Atmospheric Turbulence Transport Aircraft Systems Engineering Automatic Flight Control Automatic Pilots Aircraft Equipment Feedback Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
