Cooperative circular pattern target tracking by multiple UAVs using navigation functionNavigation 함수를 이용한 다수 무인기의 원 형태 목표물 추종 유도법칙 연구

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dc.contributor.advisorBang, Hyo-Choong-
dc.contributor.advisor방효충-
dc.contributor.authorHong, Jin-Sung-
dc.date.accessioned2019-08-25T02:49:12Z-
dc.date.available2019-08-25T02:49:12Z-
dc.date.issued2018-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=828248&flag=dissertationen_US
dc.identifier.urihttp://hdl.handle.net/10203/265406-
dc.description학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2018.8,[v, 75 p. :]-
dc.description.abstractIf the UAVs measure only the range from the target in a two-dimensional space and the range sensor has the minimum error covariance at some distance from the target (the so-called sweet spot), then an optimal configuration is the one in which the UAVs are uniformly placed in a circular fashion around the target. The determinant of the Fisher Information Matrix (FIM) is very sensitive to changes in range but exhibits far less sensitivity to changes in angular separation. If the gradient descent method using the FIM is employed, which is considered an appropriate algorithm for real-time applications, it first reduces the range as much as possible. It results in the UAV configuration at the same distance from the target, but not in evenly spaced positions according to the initial condition. From the point of view of information, the optimal position of UAVs for minimizing the uncertainties of the target information is evenly spaced positions around the target. Our study proved that the proposed guidance law made multiple UAVs to be deployed at the optimal positions. To prove the validity of the proposed guidance law, the results were compared with the previous approach, which considered specific conditions because such an observation helped us to anticipate how the guidance law works properly. From a simulation with ten UAVs which started from random positions, it was verified that the proposed guidance law steered the UAVs to the sweet spot in evenly spaced locations. It was also showed that ten UAVs never collided with each other and automatically maximized the Fisher Information Matrix.-
dc.languageeng-
dc.publisher한국과학기술원-
dc.subjectMultiple UAVs▼anavigation function▼afisher information matrix▼acircular pattern guidance-
dc.subject다수 무인기▼a네비게이션 함수▼a피셔 정보 매트릭스▼a원 형태 유도법칙-
dc.titleCooperative circular pattern target tracking by multiple UAVs using navigation function-
dc.title.alternativeNavigation 함수를 이용한 다수 무인기의 원 형태 목표물 추종 유도법칙 연구-
dc.typeThesis(Ph.D)-
dc.identifier.CNRN325007-
dc.description.department한국과학기술원 :항공우주공학과,-
dc.contributor.alternativeauthor홍진성-
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