Flight control design for a flexible conceptual aircraft using backstepping technique
A nonlinear flight control system is proposed for a conceptual flexible aircraft using Backstepping technique to achieve global stability in the rigid and flexible dynamics. It is introduced a controller to lead the model to a rigid-body model approximation, minimizing structural dynamics effects us...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2011
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2170 |