High-Performance Adaptive Pressure Control in the Presence of Time Delays: Pressure Control for Use in Variable-Thrust Rocket Development

dc.citation.epage52en_US
dc.citation.issueNumber5en_US
dc.citation.spage26en_US
dc.citation.volumeNumber38en_US
dc.contributor.authorAlan A.en_US
dc.contributor.authorYildiz, Y.en_US
dc.contributor.authorPoyraz U.en_US
dc.date.accessioned2019-02-21T16:04:46Z
dc.date.available2019-02-21T16:04:46Z
dc.date.issued2018en_US
dc.departmentDepartment of Mechanical Engineeringen_US
dc.description.abstractSmart defense systems using missiles that can fine-tune their velocity profiles have significant technological superiority over their conventional counterparts. This tuning is possible, in part, due to the deployment of advanced sensing, actuation, and computation capabilities and sophisticated guidance, navigation, and control algorithms. The capability to alter velocity during operation helps sustain optimum performance for different flight conditions. In addition, it makes it possible to slow down while turning and then speed up along a straight path, rendering the maneuvers more efficient. This ability to modify velocity (known as throttleability) is also known to increase a missile's no-escape zone, which is the maximum range that the missile can outrun its target [1]. As presented in »Summary,» this article discusses the advanced control technologies needed to obtain throttleability.
dc.description.provenanceMade available in DSpace on 2019-02-21T16:04:46Z (GMT). No. of bitstreams: 1 Bilkent-research-paper.pdf: 222869 bytes, checksum: 842af2b9bd649e7f548593affdbafbb3 (MD5) Previous issue date: 2018en
dc.identifier.doi10.1109/MCS.2018.2851009
dc.identifier.issn1066-033X
dc.identifier.urihttp://hdl.handle.net/11693/50208
dc.language.isoEnglish
dc.publisherInstitute of Electrical and Electronics Engineers
dc.relation.isversionofhttps://doi.org/10.1109/MCS.2018.2851009
dc.source.titleIEEE Control Systemsen_US
dc.titleHigh-Performance Adaptive Pressure Control in the Presence of Time Delays: Pressure Control for Use in Variable-Thrust Rocket Developmenten_US
dc.typeArticleen_US

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