Aircraft control law reconfiguration

    Vladislav Kosyanchuk Info
    Nikolay Selvesyuk Info
    Alexey Kulchak Info
DOI: https://doi.org/10.3846/16487788.2015.1015290

Abstract

The synthesis of MIMO fault-tolerant control systems under control failures is considered. The solution is written in an analytical form, which makes it possible to synthesize simplified circuit implementations and adjust coefficients of the fault-tolerant control system in the case of a non-stationary object. А nonlinear medium-range aircraft model was used to verify the results.

Keywords:

control systems, aircraft, air incidents, reconfiguration algorithms

How to Cite

Kosyanchuk, V., Selvesyuk, N., & Kulchak, A. (2015). Aircraft control law reconfiguration. Aviation, 19(1), 14-18. https://doi.org/10.3846/16487788.2015.1015290

Share

Published in Issue
March 30, 2015
Abstract Views
666

View article in other formats

CrossMark check

CrossMark logo

Published

2015-03-30

Issue

Section

Articles

How to Cite

Kosyanchuk, V., Selvesyuk, N., & Kulchak, A. (2015). Aircraft control law reconfiguration. Aviation, 19(1), 14-18. https://doi.org/10.3846/16487788.2015.1015290

Share