Design of Nonlinear Dynamic Inverse Control Law for High Angle of Attack Aircraft
碩士 === 國立成功大學 === 航空太空工程學系 === 107 === The purpose of this thesis is to discuss the application of Nonlinear Dynamic Inverse (NDI) in high-angle flight control. The main work is around high angle of attack (A.O.A) and the design of flight control law, so it is necessary to deal with a wide range of...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2019
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| Online Access: | http://ndltd.ncl.edu.tw/handle/9rk7bh |