Minimum-effort waypoint-following guidance

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dc.contributor.authorHe, Shaoming
dc.contributor.authorLee, Changhun
dc.contributor.authorShin, Hyosang
dc.contributor.authorTsourdos, Antonios
dc.date.accessioned2019-02-14T16:42:11Z
dc.date.available2019-02-14T16:42:11Z
dc.date.issued2019-01-30
dc.description.abstractThis paper addresses the problem of minimum-effortwaypoint-following guidance with/without arrival angle constraints of an Unmanned Aerial Vehicle. By utilizing a linearized kinematics model, the proposed guidance laws are derived as the solutions of a linear quadratic optimal control problem with an arbitrary number of terminal boundary constraints. Theoretical analysis reveals that both optimal proportional navigation guidance and trajectory shaping guidance are special cases of the proposed guidance laws. The key feature of the proposed algorithms lies in their generic property. For this reason, the guidance laws developed can be applied to general waypoint-following missions with an arbitrary number of waypoints and an arbitrary number of arrival angle constraints. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.en_UK
dc.identifier.citationHe S, Lee C-H, Shin H-Y & Tsourdos A., Minimum-effort waypoint-following guidance, Journal of Guidance, Control, and Dynamics, Early online.en_UK
dc.identifier.issn0731-5090
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/13904
dc.language.isoenen_UK
dc.publisherAIAAen_UK
dc.rightsAttribution-NonCommercial 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/*
dc.subjectAerospaceen_UK
dc.subjectAutonomous Systemsen_UK
dc.titleMinimum-effort waypoint-following guidanceen_UK
dc.typeArticleen_UK

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