Analysis of guidance laws with non-monotonic line-of-sight rate convergence

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dc.contributor.authorLee, Seokwon
dc.contributor.authorCho, Namhoon
dc.contributor.authorShin, Hyo-Sang
dc.date.accessioned2021-09-24T14:21:51Z
dc.date.available2021-09-24T14:21:51Z
dc.date.issued2021-09-20
dc.description.abstractThis study presents analyses of guidance laws that involve non-monotonic convergence in heading error from a new perspective based on an advanced stability concept. Pure proportional navigation with range-varying navigation gain is considered, and the gain condition to guarantee asymptotic convergence to the collision course is investigated while allowing the heading error to exhibit patterns that involve intermediate diversion. The extended stability criterion considered in this study allows local increase of the function in some finite intervals, which is less conservative than the standard stability theorem. The existing guidance laws involving intentional modulation of the heading error as well as the design of the navigation gain are discussed with respect to the new stability criterion.en_UK
dc.identifier.citationLee S, Cho N, Shin H-S. (2022) Analysis of guidance laws with non-monotonic line-of-sight rate convergence. IEEE Transactions on Aerospace and Electronic Systems, Volume 58, Number 2, April 2022, pp. 1029-1041en_UK
dc.identifier.issn0018-9251
dc.identifier.urihttps://doi.org/10.1109/TAES.2021.3113627
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/17104
dc.language.isoenen_UK
dc.publisherIEEEen_UK
dc.rightsAttribution-NonCommercial 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/*
dc.subjectWeaving Manoeuvreen_UK
dc.subjectObservability Enhancementen_UK
dc.subjectProportional Navigation Guidanceen_UK
dc.subjectMissile Guidanceen_UK
dc.subjectTrajectory Modulationen_UK
dc.subjectStability Theoryen_UK
dc.titleAnalysis of guidance laws with non-monotonic line-of-sight rate convergenceen_UK
dc.typeArticleen_UK

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