File Download

There are no files associated with this item.

  • Find it @ UNIST can give you direct access to the published full text of this article. (UNISTARs only)
Related Researcher

오현동

Oh, Hyondong
Autonomous Systems Lab.
Read More

Views & Downloads

Detailed Information

Cited time in webofscience Cited time in scopus
Metadata Downloads

Full metadata record

DC Field Value Language
dc.citation.conferencePlace SW -
dc.citation.conferencePlace Linkoping -
dc.citation.endPage 77 -
dc.citation.startPage 72 -
dc.citation.title 2017 Workshop on Research, Education and Development of Unmanned Aerial Systems, RED-UAS 2017 -
dc.contributor.author Jeong, Junho -
dc.contributor.author Yu, Beomyeol -
dc.contributor.author Kim, Taegyun -
dc.contributor.author Kim, Seungkeun -
dc.contributor.author Suk, Jinyoung Suk -
dc.contributor.author Oh, Hyondong -
dc.date.accessioned 2023-12-19T18:09:52Z -
dc.date.available 2023-12-19T18:09:52Z -
dc.date.created 2018-01-05 -
dc.date.issued 2017-10-03 -
dc.description.abstract This paper proposes a decoy application using a ducted-fan flight array system which composes of multiple single modules. Each single module has a conventional ducted-fan configuration and can fly individually. For the single module and the connected array, kinematic and dynamic models are briefly introduced. Based on the derived models, a control system is built into a hierarchical structure based on the SMC and PID methods. Also, simple kinematics is applied for multiple ASM and a target ship. A PNG law is designed for the guided missile system. Furthermore, a sequential logic proposed to take account of an expected signal power (ESP) for the deployment strategy. The ESP is calculated using seeker and decoy signal models at a control station, and then the station sends path planning commands to the multiple decoys. A numerical simulation is conducted under the visualization environment and verifies the decoy mission with two missiles and two decoys. The simulation shows that the separated single modules fulfill the role of the decoy effectively to counteract the multiple ASMs. -
dc.identifier.bibliographicCitation 2017 Workshop on Research, Education and Development of Unmanned Aerial Systems, RED-UAS 2017, pp.72 - 77 -
dc.identifier.doi 10.1109/RED-UAS.2017.8101646 -
dc.identifier.scopusid 2-s2.0-85047641183 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/35257 -
dc.identifier.url http://ieeexplore.ieee.org/document/8101646/ -
dc.language 영어 -
dc.publisher 2017 Workshop on Research, Education and Development of Unmanned Aerial Systems, RED-UAS 2017 -
dc.title Maritime application of ducted-fan flight array system: decoy for anti-ship missile -
dc.type Conference Paper -
dc.date.conferenceDate 2017-10-03 -

qrcode

Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.