Adaptive Output Feedback Based on Closed-Loop Reference Models for Hypersonic Vehicles
This paper presents a new method of synthesizing an output feedback adaptive controller for a class of uncertain, non-square, multi-input multi-output systems that often occur in hypersonic vehicle models. The main challenge that needs to be addressed is the determination of a corresponding square a...
| Main Authors: | , , , , |
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| Language: | en_US |
| Published: |
2016
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| Online Access: | http://hdl.handle.net/1721.1/101648 |