Resonance control of aircraft instabilities by smooth and continuous feedback

DOI10.2514/3.21545zbMath0840.93066OpenAlexW2063873309MaRDI QIDQ4864418

Bill Essary, Mark A. Pinsky

Publication date: 7 March 1996

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.21545

zbMATH Keywords

bifurcationnormal formshigh angle-of-attack aircraftsmooth nonlinear feedback

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15) Application models in control theory (93C95) Control/observation systems governed by ordinary differential equations (93C15)

This page was built for publication: Resonance control of aircraft instabilities by smooth and continuous feedback