Robustness margin for attitude control of a four rotor mini-rotorcraft: Case of study

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2009-12-18

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Elsevier BV

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Robustness (evolution), Control theory (sociology), Parametric statistics, Robust control, Helicopter rotor, Engineering, Multivariable calculus, Attitude control, Complex plane, Control system, Control engineering, Computer science

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https://riuat.uat.edu.mx/handle/123456789/2553

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Except where otherwise noted, this item's license is described as Acceso restringido / Suscripción (Metadatos de producción científica)