Bifurcation Analysis and Control of High Angle-of-Attack Flight Dynamics
碩士 === 國立交通大學 === 控制工程系 === 82 === In order to increase the performance of aircraft, the modern aircraft is being designed for maneuvering at high angle-of- attack. The flight of high angle-of-attack offers a substantial increase in agility...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
1994
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| Online Access: | http://ndltd.ncl.edu.tw/handle/70771404982000981733 |