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Uh-60 black hawk disturbance rejection study for hover/low speed handling qualities criteria and turbulence modeling
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Blanken, Chris L. Tischler, Mark B. Labows, Steven J. |
| Copyright Year | 1999 |
| Description | This paper will discuss the airborne flight test of the Sikorsky UH-60 Black Hawk helicopter in turbulent conditions to determine disturbance rejection criteria and develop a low speed wind/turbulence model for helicopter simulation. |
| File Size | 252013 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20000090530 |
| Archival Resource Key | ark:/13960/t7rn83j5z |
| Language | English |
| Publisher Date | 1999-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests Low Speed Stability Control Simulation Turbulence Flight Conditions Helicopters Helicopter Control Motion Simulation Hovering Stability Maneuverability Controllability Helicopter Performance Flight Simulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
