MATEC Web Conf.
Volume 99, 20172016 Workshop on Contemporary Materials and Technologies in the Aviation Industry (CMTAI2016)
|Number of page(s)||3|
|Section||Guidance, Navigation and Control|
|Published online||08 February 2017|
Quantitative Model-Free Method for Aircraft Control System Failure Detection
FGUP “GosNIIAS”, 125319 Moscow, Russia
* Corresponding author: firstname.lastname@example.org
The problem of the failure detection in the aircraft control system in the presence of disturbance is considered. A history based model-free nonstatistical method using the aircraft control and state data measurements only is proposed. The method needs no a priori information about the model of an aircraft, solving the prediction, identification and training problems.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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