An adaptive pitch axis autopilot design for an unstable nonminimum phase pitch axis model
An adaptive pitch axis autopilot design procedure is presented. The design procedure is applicable to both stable and unstable pitch axis models and to those having nonminimum phase. The design approach assumes the adaptive autopilot is activated after achieving level flight. It is shown a rate-feed...
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| Language: | en_US |
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2013
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| Online Access: | http://hdl.handle.net/1957/38014 |