Titreşim Temelli Uydu Yönelim Denetimi Eyleyicisi Kavramsal Doğrulaması

Date

2019-01-01

Author

Tekinalp, Ozan
Azgın, Kıvanç

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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Bu projede özgün salınımlı rotor ve yalpalayan çubuk tipi prototip yönelim kontrol eyleyicileri gelistirilmistir. Öncelikle eyleyicilerin uydu yönelimine etkileri matematiksel olarak modellenmistir. Daha sonra olusturulan matematik modelden çıkarımlar yapılarak tasarım yaklasımları belirlenmis ve eyleyici tasarımları yapılmıstır. Yük hücresi ve dijital-analog dönüstürücü kartlarından olusan deneysel bir düzenekten faydalanarak eyleyicilerin çalısması kaynaklı kuvvet ve moment degerleri ölçülmüstür. Ayrıca tek eksenli bir hava yatagı kullanılarak da deneyler gerçeklestirilmistir ve eyleyicilerin uydu yönelimindeki basarısı gösterilmistir. Yine özgün yalpalayan çubuk temelli mikro elektromekanik seviyesi eyleyici tasarımı da yapılmıstır.

Subject Keywords

Uydu yönelim kontrolü, uydu eyleyicisi, yalpalayan çubuk, mikro elektromekanik eyleyici, çip uydu

URI

https://hdl.handle.net/11511/95864

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Department of Aerospace Engineering, Project and Design

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Citation Formats

O. Tekinalp and K. Azgın, “Titreşim Temelli Uydu Yönelim Denetimi Eyleyicisi Kavramsal Doğrulaması,” 2019. Accessed: 00, 2022. [Online]. Available: https://hdl.handle.net/11511/95864.