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Nonlinear Model-Predictive Integrated Missile Control and Its Multiobjective Tuning

2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 11 Linguagem: Inglês

10.2514/1.g002279

1533-3884

Vincent Bachtiar, Chris Manzie, Eric C. Kerrigan,

Rocket and propulsion systems research

No AccessEngineering NoteNonlinear Model-Predictive Integrated Missile Control and Its Multiobjective TuningVincent Bachtiar, Chris Manzie and Eric C. KerriganVincent BachtiarUniversity of Melbourne, Melbourne, Victoria 3010, Australia, Chris ManzieUniversity of Melbourne, Melbourne, Victoria 3010, Australia and Eric C. KerriganImperial College London, London, England SW7 2AZ, United KingdomPublished Online:4 Jul 2017https://doi.org/10.2514/1.G002279SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Menon P. and Ohlmeyer E., "Integrated Design of Agile Missile Guidance and Autopilot Systems," Control Engineering Practice, Vol. 9, No. 10, 2001, pp. 1095–1106. doi:https://doi.org/10.1016/S0967-0661(01)00082-X COEPEL 0967-0661 CrossrefGoogle Scholar[2] Menon P., Sweriduk G., Ohlmeyer E. and Malyevac D., "Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads," Journal of Guidance, Control, and Dynamics, Vol. 27, No. 1, 2004, pp. 118–126. doi:https://doi.org/10.2514/1.9336 LinkGoogle Scholar[3] Levy M., Shima T. and Gutman S., "Linear Quadratic Integrated Versus Separated Autopilot-Guidance Design," Journal of Guidance, Control, and Dynamics, Vol. 36, No. 6, 2013, pp. 1722–1730. doi:https://doi.org/10.2514/1.61363 LinkGoogle Scholar[4] Idan M., Shima T. and Golan O. 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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 TheoryCruise MissilesGuidance, Navigation, and Control SystemsMilitary ScienceMilitary TechnologyMissile DefenseMissile Guidance and ControlMissile Systems, Dynamics and TechnologyMissilesNavigational GuidanceWeapon Systems KeywordsMissile GuidanceModel Predictive ControlSequential Quadratic ProgrammingAutopilotAngle of AttackAerodynamic CoefficientsControl AlgorithmParticle Swarm OptimizationInertial Measurement UnitProportional NavigationPDF Received6 June 2016Accepted25 April 2017Published online4 July 2017