Aircraft control using nonlinear dynamic inversion in conjunction with adaptive robust control
This thesis describes the implementation of Yaos adaptive robust control to an aircraft control system. This control law is implemented as a means to maintain stability and tracking performance of the aircraft in the face of failures and changing aerodynamic response. The control methodology is imp...
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| Format: | Others |
| Language: | en_US |
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Texas A&M University
2005
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| Online Access: | http://hdl.handle.net/1969.1/1515 |