Optimality of Error Dynamics in Missile Guidance Problems
2018; American Institute of Aeronautics and Astronautics; Volume: 41; Issue: 7 Linguagem: Inglês
10.2514/1.g003343
ISSN1533-3884
Autores Tópico(s)Adaptive Control of Nonlinear Systems
ResumoNo AccessEngineering NoteOptimality of Error Dynamics in Missile Guidance ProblemsShaoming He and Chang-Hun LeeShaoming HeCranfield University, Cranfield, England MK43 0AL, United Kingdom and Chang-Hun LeeCranfield University, Cranfield, England MK43 0AL, United KingdomPublished Online:22 Feb 2018https://doi.org/10.2514/1.G003343SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Murtaugh S. A. and Criel H. E., "Fundamentals of Proportional Navigation," IEEE Spectrum, Vol. 3, No. 12, 1966, pp. 75–85. doi:https://doi.org/10.1109/MSPEC.1966.5217080 IEESAM 0018-9235 CrossrefGoogle Scholar[2] Zarchan P., Tactical and Strategic Missile Guidance, AIAA, Reston, VA, 2012, pp. 163–184. 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All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAvionicsControl TheoryGuidance, Navigation, and Control SystemsGuided MissilesHoming GuidanceMilitary ScienceMilitary TechnologyMissile Guidance and ControlMissile Systems, Dynamics and TechnologyMissilesNavigational GuidanceSurface-to-Air MissileWeapon Systems KeywordsMissile GuidanceControl GuidanceFlight Path AngleSliding Mode ControlAngle of AttackEngagement KinematicsAutopilotMissile DynamicsNonlinear ControlOptimal ControlPDF Received5 October 2017Accepted10 January 2018Published online22 February 2018
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