Satellite attitude control by integrator back-stepping with internal stabilization

Date

2008-01-01

Author

Doruk, Resat Oezguer
Kocaoglan, Erol

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

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Purpose - This paper aims to focus on the implementation of the integral back-stepping control on the model of BILSAT - 1 satellite of the Turkish Scientific and Technological Research Council (TUBITAK).

Subject Keywords

Control, Artificial satellites

URI

https://hdl.handle.net/11511/65229

Journal

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY

DOI

https://doi.org/10.1108/00022660810841958

Collections

Department of Electrical and Electronics Engineering, Article

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Citation Formats

R. O. Doruk and E. Kocaoglan, “Satellite attitude control by integrator back-stepping with internal stabilization,” AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, pp. 3–10, 2008, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/65229.