Analysis of rendezvous guidance laws for autonomous aerial refueling for non-maneuvering and identical speed targets

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dc.contributor.authorLee, Seokwon
dc.contributor.authorKim, Mingu
dc.date.accessioned2022-01-21T14:05:25Z
dc.date.available2022-01-21T14:05:25Z
dc.date.issued2022-01-14
dc.description.abstractThis study analyzes rendezvous guidance schemes for UAVs refueling. Assuming the target is non-maneuvering with identical speed, a necessary condition is investigated for the UAV to approach the rendezvous point. Three types of guidance laws are considered to analyze the performance under the condition. A reachable region is analytically obtained using the closed-form solution of the deviated pursuit and pure proportional navigation. Numerical simulation demonstrates the analyzed result for the rendezvous mission.en_UK
dc.identifier.citationLee S, Kim M. (2022) Analysis of rendezvous guidance laws for autonomous aerial refueling for non-maneuvering and identical speed targets. Aerospace Science and Technology, Volume 121, February 2022, Article number 107359en_UK
dc.identifier.issn1270-9638
dc.identifier.urihttps://doi.org/10.1016/j.ast.2022.107359
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/17472
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectRendezvous Guidanceen_UK
dc.subjectAir-to-Air Refuelingen_UK
dc.subjectDeviated Pursuit Guidanceen_UK
dc.subjectProportional Navigation Guidanceen_UK
dc.titleAnalysis of rendezvous guidance laws for autonomous aerial refueling for non-maneuvering and identical speed targetsen_UK
dc.typeArticleen_UK

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