dc.contributor.author | Bručas, Domantas | |
dc.contributor.author | Bansevičius, Ramutis Petras | |
dc.contributor.author | Domeika, Aurelijus | |
dc.contributor.author | Tomkus, Vidmantas | |
dc.contributor.author | Bakanauskas, Vytautas | |
dc.date.accessioned | 2023-09-18T17:32:01Z | |
dc.date.available | 2023-09-18T17:32:01Z | |
dc.date.issued | 2012 | |
dc.identifier.issn | 1392-8716 | |
dc.identifier.other | (BIS)KTU02-000048345 | |
dc.identifier.uri | https://etalpykla.vilniustech.lt/handle/123456789/124114 | |
dc.description.abstract | In recent years a very modern trend of space exploration activities – constructing, launching and operating nano-satellites, became very popular. One of the main problems in implementation and control of nano-satellite is ensuring accurate yet simple and small-sized attitude control equipment. Most of the equipment implemented for that task in the past was large, bulky and could be hardly used on extremely small CubeSat standard nano-satellites. The equipment under development for attitude control of the satellites is described in this paper. The equipment relies on implementation of piezoelectric transducers for rotation of spherical body – reaction sphere, thus ensuring precise three-axis attitude control of the satellite by means of single device. Description of the device under development with some calculations and examples of implementation of such instrumentation is further described in the paper. | eng |
dc.format.extent | p. 1246-1251 | |
dc.format.medium | tekstas / txt | |
dc.language.iso | eng | |
dc.relation.isreferencedby | Science Citation Index Expanded (Web of Science) | |
dc.relation.isreferencedby | Scopus | |
dc.relation.isreferencedby | INSPEC | |
dc.relation.isreferencedby | Computers & Applied Sciences Complete | |
dc.relation.isreferencedby | Academic Search Complete | |
dc.relation.isreferencedby | Central & Eastern European Academic Source (CEEAS) | |
dc.relation.isreferencedby | DOAJ | |
dc.rights | Laisvai prieinamas internete | |
dc.source.uri | https://talpykla.elaba.lt/elaba-fedora/objects/elaba:3217788/datastreams/MAIN/content | |
dc.title | Novel attitude control devices for CubeSat satellites | |
dc.type | Straipsnis Web of Science DB / Article in Web of Science DB | |
dcterms.license | Creative Commons – Attribution – 4.0 International | |
dcterms.references | 12 | |
dc.type.pubtype | S1 - Straipsnis Web of Science DB / Web of Science DB article | |
dc.contributor.institution | Vilniaus Gedimino technikos universitetas | |
dc.contributor.institution | Kauno technologijos universitetas | |
dc.contributor.institution | Lietuvos kosmoso asociacija | |
dc.contributor.faculty | Antano Gustaičio aviacijos institutas / Antanas Gustaitis Aviation Institute | |
dc.subject.researchfield | T 003 - Transporto inžinerija / Transport engineering | |
dc.subject.researchfield | T 009 - Mechanikos inžinerija / Mechanical enginering | |
dc.subject.researchfield | T 010 - Matavimų inžinerija / Measurement engineering | |
dc.subject.en | Nano-satellite | |
dc.subject.en | CubeSat | |
dc.subject.en | Attitude control | |
dc.subject.en | Reaction-wheel | |
dc.subject.en | Momentum of inertia | |
dcterms.sourcetitle | Journal of Vibroengineering | |
dc.description.issue | iss. 3 | |
dc.description.volume | vol. 14 | |
dc.publisher.name | Vibromechanika | |
dc.publisher.city | Vilnius | |
dc.identifier.doi | VGT02-000025271 | |
dc.identifier.doi | 000309037800033 | |
dc.identifier.doi | 1 | |
dc.identifier.elaba | 3217788 | |