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Aircraft load alleviation by robust yaw-lateral decoupling. - MaRDI portal

Aircraft load alleviation by robust yaw-lateral decoupling.

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Publication:1421415

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DOI10.1016/S0005-1098(03)00218-8zbMath1044.93049MaRDI QIDQ1421415

Jürgen Ackermann, Michael Kordt

Publication date: 26 January 2004

Published in: Automatica (Search for Journal in Brave)

zbMATH Keywords

aircraft disturbance compensation load alleviation pilot delay robust decoupling vertical tail

Mathematics Subject Classification ID

Application models in control theory (93C95) Perturbations in control/observation systems (93C73)

Cites Work

Robust flight control. A design challenge

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