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Three Dimensional Path Planning and Guidance for Aerial Refueling of Unmanned Aerial Vehicle : 무인기 공중급유를 위한 3차원 경로계획 및 유도기법

DC Field Value Language
dc.contributor.advisor김유단-
dc.contributor.author윤유정-
dc.date.accessioned2017-07-14T03:43:25Z-
dc.date.available2017-07-14T03:43:25Z-
dc.date.issued2017-02-
dc.identifier.other000000140629-
dc.identifier.urihttps://hdl.handle.net/10371/123920-
dc.description학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2017. 2. 김유단.-
dc.description.abstractIn this thesis, a rendezvous path planning is considered for a UAV (Un-manned Aerial Vehicle). The objective of the path planning is to make the tanker and the UAV perform rendezvous at a pre-planned point, and then the UAV should maintain the same speed with the tanker to accomplish aerial refueling mission. Since the aerial refueling mission is generally per-formed between one tanker and multiple aircraft, setting the pre-planned point for the rendezvous will be efficient in the operation management level. In this study, rendezvous path planning and guidance law are pro-posed such that the UAV can be prevented from turning sharply while minimizing an energy consumption. Numerical simulations are performed for rendezvous and aerial refueling mission to demonstrate the perfor-mance of the proposed path planning and guidance law.-
dc.description.tableofcontents1 Introduction 1
1.1 Background 1
1.2 Related Research 2
1.3 Contributions 4
1.4 Thesis Organization 5
2 Guidance Laws for UAV Rendezvous 6
2.1 Pure pursuit guidance law 6
2.2 Proportional navigation guidance law 8
2.3 PP guidance law and PN guidance law 9
3 Rendezvous Path Planning in Two Dimensions 10
3.1 Path planning 10
3.2 Approach phase 11
3.2.1 Pseudo pursuit guidance law 11
3.2.2 Transition around the CTA 13
3.2.3 Determination of UAV initial velocity range 15
3.3 Rendezvous phase 23
3.3.1 Velocity control for the rendezvous 24
4 Rendezvous Path Planning in Three Dimensions 27
4.1 Approach phase 27
4.2 Velocity optimization to minimize energy consumption 30
4.3 Rendezvous phase 32
4.4 Pseudo pursuit guidance vs. straight climb in the approach phase 33
5 Numerical Simulations 35
5.1 Simulation Environment 35
5.2 Simulation Results 37
5.2.1 Single UAV case 37
5.2.2 Multiple UAVs case 42
6 Conclusions 50
6.1 Concluding Remarks 50
6.2 Future Work 50
References 52
국문초록 55
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dc.formatapplication/pdf-
dc.format.extent4213733 bytes-
dc.format.mediumapplication/pdf-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subjectRendezvous-
dc.subjectPursuit guidance law-
dc.subjectAerial refueling-
dc.subjectUnmanned Aerial Vehicle-
dc.subject.ddc621-
dc.titleThree Dimensional Path Planning and Guidance for Aerial Refueling of Unmanned Aerial Vehicle-
dc.title.alternative무인기 공중급유를 위한 3차원 경로계획 및 유도기법-
dc.typeThesis-
dc.contributor.AlternativeAuthorYujung Yoon-
dc.description.degreeMaster-
dc.citation.pagesvii, 55-
dc.contributor.affiliation공과대학 기계항공공학부-
dc.date.awarded2017-02-
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