Aircraft simulation and control
This dissertation aims at F-16 fighter to design controller and to make simulation for analyzing its performance under specific condition. Nonlinear plants model of F-16 derived from the kinematics and dynamics of aircraft is first given, which provides a necessary precondition for analyzing and res...
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| Format: | Thesis |
| Language: | English |
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2009
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| Online Access: | http://hdl.handle.net/10356/18758 |