Aircraft control law reconfiguration
DOI: https://doi.org/10.3846/16487788.2015.1015290Abstract
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 algorithmsHow 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
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Copyright (c) 2015 The Author(s). Published by Vilnius Gediminas Technical University.
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Published
2015-03-30
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Copyright
Copyright (c) 2015 The Author(s). Published by Vilnius Gediminas Technical University.
License
This work is licensed under a Creative Commons Attribution 4.0 International License.
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