Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts
This thesis provides background, theory, and examples for a high performance fighter aircraft (a modified model of F-16) control design. There are mainly three parts in this thesis. The first part presents the development of a software package for flight simulation of a high performance fighter airc...
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| Format: | Theses and Dissertations |
| Language: | English |
| Published: |
2009
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| Online Access: | http://hdl.handle.net/10356/19603 |
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| Institution: | Nanyang Technological University |
| Language: | English |