Impact time control based on time-to-go prediction for sea-skimming antiship missiles

dc.contributor.authorTahk, Min-Jea
dc.contributor.authorShim, Sang-Wook
dc.contributor.authorHong, Seong-Min
dc.contributor.authorChoi, Han-Lim
dc.contributor.authorLee, Chang-Hun
dc.date.accessioned2018-09-25T10:14:37Z
dc.date.available2018-09-25T10:14:37Z
dc.date.issued2018-02-07
dc.description.abstractThis paper proposes a novel approach for guidance law design to satisfy the impact-time constraints for a certain class of homing missiles. The proposed guidance law provides proper lateral acceleration commands that make the impact time error converge to zero by the time of impact. This scheme can be applied to any existing guidance law for which a formula of predicted time to go is available. Convergence of time-to-go errors is supported by Lyapunov stability. The optimal guidance law and the impact angle control guidance law are extended by the proposed method for impact-time-control guidance and impact-time-and-angle-control guidance, respectively. The performance of the extended guidance laws is demonstrated by numerical simulation.en_UK
dc.identifier.citationMin-Jea Tahk, Sang-Wook Shim, Seong-Min Hong, et al., Impact time control based on time-to-go prediction for sea-skimming antiship missiles. IEEE Transactions on Aerospace and Electronic Systems, Volume 54, Issue 4, August 2018, pp. 2043-2052en_UK
dc.identifier.issn0018-9251
dc.identifier.urihttps://doi.org/10.1109/TAES.2018.2803538
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/13485
dc.language.isoenen_UK
dc.publisherIEEEen_UK
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.titleImpact time control based on time-to-go prediction for sea-skimming antiship missilesen_UK
dc.typeArticleen_UK

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