| Property | Value |
| Name | Variable-Structure Control of a Model Glider Airplane |
| Description | It has long been known that the most effective spin recovery technique for fuselage-heavy aircraft is to use the ailerons to roll the aircraft into the spin. The objective of this paper is to explore this well-known spin recovery strategy using a recently-developed integrated toolset for modeling and analysis of highly dynamic aircraft motions. |
| Filename | LAR17106-1.pdf |
| Filesize | 222.71 kB |
| Filetype | pdf (Mime Type: application/pdf) |
| Creator | selinsky |
| Created On: | 07/01/2008 10:04 |
| Viewers | Everybody |
| Maintained by | Editor |
| Hits | 17 Hits |
| Last updated on | 06/30/2008 10:08 |
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