High-precision control of nonstationary aircrafts by roll angle

DOI10.1134/S0005117913050111zbMath1268.93057OpenAlexW2054075195MaRDI QIDQ2393026

V. M. Sukhanov, V. M. Glumov, V. Yu. Rutkovskii

Publication date: 7 August 2013

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0005117913050111

zbMATH Keywords

control algorithmsparametric disturbanceshigh-precision controlroll angleadditional adaptive control loopnonstationary aircrafts

Mathematics Subject Classification ID

Adaptive control/observation systems (93C40) Perturbations in control/observation systems (93C73) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• A physically realizable precision control algorithm for a nonstationary dynamic object
• Physically realizable reference model-based algorithm of adaptive control
• Precision control algorithm for a dynamic system under uncertainty based on an adaptive system with a reference model
• On the Stability of Nonautonomous Differential Equations $\dot x = [A + B(t)x$, with Skew Symmetric Matrix $B(t)$]

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