Flight control design using non-linear inverse dynamics

DOI10.1016/0005-1098(88)90092-1zbMath0649.93051OpenAlexW2088709416MaRDI QIDQ1106171

Robert F. Stengel, Stephen H. Lane

Publication date: 1988

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0005-1098(88)90092-1

zbMATH Keywords

Flight control systemsnon-linear inverse dynamics

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Application models in control theory (93C95) General aerodynamics and subsonic flows (76G25) Synthesis problems (93B50) Control/observation systems governed by ordinary differential equations (93C15)

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Cites Work

• Unnamed Item
• Application of nonlinear transformations to automatic flight control
• Nonlinear flight test trajectory controllers for aircraft
• Output feedback non-linear decoupled control synthesis and observer design for manoeuvring aircraft
• The structure of decoupled non-linear systems

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