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Space shuttle pilot-induced-oscillation research testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Powers, B. G. |
| Copyright Year | 1984 |
| Description | The simulation requirements for investigation of pilot-induced-oscillation (PIO) characteristics during the landing phase are discussed. Orbiters simulations and F-8 digital fly-by-wire aircraft tests are addressed. |
| File Size | 395994 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840012498 |
| Archival Resource Key | ark:/13960/t02z62m83 |
| Language | English |
| Publisher Date | 1984-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Pilot Performance F-8 Aircraft Fly By Wire Control Oscillations Pilot Induced Oscillation Computerized Simulation Space Shuttle Orbiters Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |