On unsteady aerodynamic airfoil loads in the design of a control system for minimizing the effect of wind perturbations using the rudder on the trailing edge of the wing

DOI10.1134/S1064230706050121zbMath1263.93236OpenAlexW1980967435MaRDI QIDQ1951897

A. N. Khrabrov, M. G. Goman, M. E. Sidoryuk

Publication date: 24 May 2013

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230706050121

Mathematics Subject Classification ID

Application models in control theory (93C95) Perturbations in control/observation systems (93C73) Optimal stochastic control (93E20)

Uses Software

• LMI toolbox
• Control System Toolbox
• Mu Analysis and Synthesis Toolbox
• Unnamed Item

Cites Work

• Mathematical modeling of time-dependent aerodynamic loads on an airfoil with dynamic deflection of a control on the trailing edge
• All optimal Hankel-norm approximations of linear multivariable systems and theirL,^∞-error bounds†
• State-space solutions to standard H/sub 2/ and H/sub infinity / control problems
• A convex characterization of gain-scheduled H/sub ∞/ controllers

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