Publication:
Trajectory tracking of a satellite communicated missile with Fuzzy and PID control

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dc.contributor.authorsYagimli M., Simsir U., Tozan H.
dc.date.accessioned2022-03-15T01:58:42Z
dc.date.accessioned2026-01-11T13:29:57Z
dc.date.available2022-03-15T01:58:42Z
dc.date.issued2011
dc.description.abstractIn this study, the trajectory of a satellite communicated missile, which is thrown from combat plane to combat plane, has been investigated with using Fuzzy and PID control seperately. The Guidance Section of Missile consists of an active radar seeker and radome, radar altimeter and antennas, and power converter. Simulations have been done with Matlab Simulink toolbox and utilized standard transfer function of missile on block diagram. The results, enabled with PID and Fuzzy Control, have been compared and given in this study. © 2011 IEEE.
dc.identifier.doi10.1109/RAST.2011.5966848
dc.identifier.isbn9781424496143
dc.identifier.urihttps://hdl.handle.net/11424/247105
dc.language.isoeng
dc.relation.ispartofRAST 2011 - Proceedings of 5th International Conference on Recent Advances in Space Technologies
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectfuzzy control
dc.subjectmissile
dc.subjectPID control
dc.subjecttrajectory tracking
dc.titleTrajectory tracking of a satellite communicated missile with Fuzzy and PID control
dc.typeconferenceObject
dspace.entity.typePublication
oaire.citation.endPage323
oaire.citation.startPage318
oaire.citation.titleRAST 2011 - Proceedings of 5th International Conference on Recent Advances in Space Technologies

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