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Aircraft control law reconfiguration

    Vladislav Kosyanchuk Affiliation
    ; Nikolay Selvesyuk Affiliation
    ; Alexey Kulchak Affiliation
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.

Keyword : 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
Published in Issue
Mar 30, 2015
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This work is licensed under a Creative Commons Attribution 4.0 International License.