Zobrazeno 1 - 10
of 30
pro vyhledávání: '"NON LINEAR GEOMETRIC APPROACH"'
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9783642393471
This contribution describes the application of differential geometry and nonlinear systems analysis to the estimation of friction effects in a class of mechanical systems. The proposed methodology, that has been developed for the more general problem
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4d6234110ae0bd151036b0e1ea307000
http://hdl.handle.net/11585/255280
http://hdl.handle.net/11585/255280
Kniha
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Publikováno v:
Advances in Condition Monitoring of Machinery in Non-Stationary Operations; 2014, p355-365, 11p
Publikováno v:
IFAC Proceedings Volumes. 45:1095-1100
This paper presents new results regarding the development of a fault detection and isolation scheme for a nonlinear satellite model. The main issue concerns the handling of frequency faults affecting the reaction wheels of a spacecraft attitude contr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::42edd139afe472915d390d0ff63eb8aa
https://doi.org/10.3182/20120829-3-mx-2028.00178
https://doi.org/10.3182/20120829-3-mx-2028.00178
This paper proposes a solution to the aircraft control problem during landing phases in presence of microburst wind shear. This work addresses the design of an adaptive controller which, exploiting the wind estimation provided by suitable filters, im
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1cc6aed95f5cea7b698d44f25abd1c2b
http://hdl.handle.net/11392/2036812
http://hdl.handle.net/11392/2036812
This work shows how to use a differential geometry tool to design a novel nonlinear active fault tolerant flight control system for aircraft. The proposed control scheme consists of two main subsystems: a controller, which is designed for the nominal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3244734a4a55d07f5f0972b243233b44
http://hdl.handle.net/11585/255489
http://hdl.handle.net/11585/255489
In this work, different procedures for sensor Fault Detection and Isolation (FDI) applied to a simulated model of a commercial aircraft are presented. The main point of the paper regards the design of two FDI schemes based on a linear Polynomial Meth
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c7db1c9d6af8c94b9b27a69bdda5715b
http://hdl.handle.net/11585/64155
http://hdl.handle.net/11585/64155
Akademický článek
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Publikováno v:
European Journal of Control; Jan2020, Vol. 51, p76-94, 19p
Design of sensor and actuator fault tolerant control system on wind turbine benchmark for Region II.
Autor:
Indriawati, Katherin1 (AUTHOR) katherin@ep.its.ac.id, Widjiantoro, Bambang L.1 (AUTHOR), Musyafa, Ali1 (AUTHOR)
Publikováno v:
AIMS Energy. 2019, Vol. 7 Issue 2, p111-126. 16p.