Cold gas thruster and controller development for satellite attitude control

dc.contributor.advisor Koyuncu, Emre
dc.contributor.author Sedaki, Hüda
dc.contributor.authorID 514211038
dc.contributor.department Defence Technologies
dc.date.accessioned 2025-07-16T09:03:41Z
dc.date.available 2025-07-16T09:03:41Z
dc.date.issued 2024-06-13
dc.description Thesis (M.Sc.) -- Istanbul Technical University, Graduate School, 2024
dc.description.abstract This paper summarizes the design and application of a cold gas thruster propulsion system for attitude control of satellites and space tugs. The control algorithm's development relies on analyzing data collected through several tests intended for system identification. Therefore, the project highlights the importance of performing real time testing on the physical system along with validating the simulation of the mathematical model. The control mainly relies on PWM signal customized under the special constraints defined by the cold gas thruster characteristics.
dc.description.degree M.Sc.
dc.identifier.uri http://hdl.handle.net/11527/27584
dc.language.iso en_US
dc.publisher Graduate School
dc.sdg.type Goal 9: Industry, Innovation and Infrastructure
dc.subject satellite control
dc.subject uydu kontrolü
dc.subject cold gas thruster
dc.subject soğuk gaz iticisi
dc.title Cold gas thruster and controller development for satellite attitude control
dc.title.alternative Soğuk gaz itki sistemin aracılığıyla uyudu yönelim kontrollü
dc.type Master Thesis
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