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Fault Tolerant Control of Attitude Dynamics of Nanosatellites

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dc.contributor.authorGuler, Demet Cilden
dc.contributor.authorHajiyev, Chingiz
dc.contributor.authorDasdemir, Janset
dc.date.accessioned2026-06-27T13:58:41Z
dc.date.issued2017
dc.description.abstractIn this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced, and the nontraditional Kalman filter is designed with the presented control algorithms. Re-adjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman Filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.en
dc.description.sponsorshipScientific and Technological Research Council of Turkey (TUBITAK) [113E595]
dc.identifier.endpage353
dc.identifier.isbn978-1-5386-1605-5
dc.identifier.startpage349
dc.identifier.urihttps://hdl.handle.net/20.500.14981/56160
dc.identifier.wos000463809900062
dc.language.isoeng
dc.publisherIEEE
dc.relation.conference8th International Conference on Recent Advances in Space Technologies (RAST)
dc.relation.ispartofPROCEEDINGS OF 8TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2017)
dc.subjectnanosatellite
dc.subjectfault tolerant control
dc.subjectreconfigurable control
dc.subjectestimation
dc.subjectattitude
dc.subjectRECONFIGURABLE FLIGHT CONTROL
dc.subject2-STAGE KALMAN FILTER
dc.subjectEngineering
dc.subjectRemote Sensing
dc.titleFault Tolerant Control of Attitude Dynamics of Nanosatellites
dc.typeProceedings Paper
dspace.entity.typePublication
local.import.sourceWOS

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