Linearization-based attitude error regulation: multiplicative error case

Date

2009-01-01

Author

Doruk, R. Ozgur

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Purpose - The purpose of this paper is to design and simulate a linearized attitude stabilizer based on linear quadratic regulator theory (LQR) using the multiplicative definition of the attitude.

Subject Keywords

Artificial satellites, Controllers, Modelling, Kinematics, Space technology

URI

https://hdl.handle.net/11511/63857

Journal

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY

DOI

https://doi.org/10.1108/00022660910997856

Collections

Department of Electrical and Electronics Engineering, Article

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Citation Formats

R. O. Doruk, “Linearization-based attitude error regulation: multiplicative error case,” AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, pp. 536–540, 2009, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/63857.