Aircraft identification applied to closed loop control system design.
In the present work, the influence of maneuver design for stability derivatives of aerodynamic forces and moments identification in the performance of closed loop control systems is evaluated, where two maneuvers largely used in aeronautical industry - doublet and 3211 - are compared to a maneuver o...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2006
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=904 |