Sliding-mode control of the super maneuverable aircraft
In this thesis, A nonlinear methodology for the control of the highly maneuverable, high performance aircraft HARV (F-18) is studied by using sliding-mode control (SMC). This control law, which takes a continuous function when the input constraints are not considered, satisfies the reachability cond...
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| Language: | en_US |
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2012
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| Online Access: | http://hdl.handle.net/1957/35615 |