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공공누리This item is licensed Korea Open Government License

dc.contributor.author
정혁준
dc.contributor.author
하영국
dc.contributor.author
정한민
dc.contributor.author
황명권
dc.date.accessioned
2019-08-28T07:41:37Z
dc.date.available
2019-08-28T07:41:37Z
dc.date.issued
2014-06-22
dc.identifier.issn
1110-757X
dc.identifier.uri
https://repository.kisti.re.kr/handle/10580/14349
dc.identifier.uri
http://www.ndsl.kr/ndsl/search/detail/article/articleSearchResultDetail.do?cn=NART73356659
dc.description.abstract
The proposed control system is modular, convenient to design and verify, and easy to extend. It comprises three layers - a physical layer, a displacement control layer, and an attitude control layer. The displacement control layer considers the movement of the vehicle, while the attitude control layer controls its attitude. The physical layer deals with the physical operation of the vehicle. The two control layers use a mathematical method to provide minute step-by-step control. The proposed control system effectively combines the three layers to achieve drift stabilization.
dc.language
eng
dc.relation.ispartofseries
Journal of Applied Mathematics
dc.title
Mathematical Modeling of a Multilayered Drift-Stabilization Method for Micro-UAVs Using Inertial Navigation Unit Sensor
dc.citation.endPage
11
dc.citation.startPage
1
dc.citation.volume
2014
dc.subject.keyword
Mathematical Modeling
dc.subject.keyword
Multilayered Drift-Stabilization
dc.subject.keyword
Micro-UAV
dc.subject.keyword
Inertial Navigation
dc.subject.keyword
Sensor
Appears in Collections:
7. KISTI 연구성과 > 학술지 발표논문
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