Finite time eigenaxis rotation using quaternion feedback

Syed Muhammad Amrr; Arunava Banerjee; M. Nabi; S. Janardhanan

doi:10.1109/RAST.2017.8002933

Finite time eigenaxis rotation using quaternion feedback

Syed Muhammad Amrr, Arunava Banerjee, M. Nabi, S. Janardhanan

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

11 Scopus citations

Abstract

The attitude of the spacecraft is its angular orientation in space. Attitude control design of a satellite system is an important area of space technology. An efficient controller is required to take the satellite system to its target orientation. In some cases, the maneuver need to be completed within a finite time. This paper introduces a novel control law which achieves finite time convergence to the required orientation. The control laws are shown to converge in a finite time for the satellite system by using Lyapunov theory and are also illustrated via simulation results.

Original language	English
Title of host publication	Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017
Editors	M.F. Unal, A. Hacioglu, M.S. Yildiz, O. Altan, M. Yorukoglu
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	105-108
Number of pages	4
ISBN (Electronic)	9781538616031
DOIs	https://doi.org/10.1109/RAST.2017.8002933
State	Published - 4 Aug 2017
Externally published	Yes
Event	8th International Conference on Recent Advances in Space Technologies, RAST 2017 - Istanbul, Turkey Duration: 19 Jun 2017 → 22 Jun 2017

Publication series

Name	Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017

Conference

Conference	8th International Conference on Recent Advances in Space Technologies, RAST 2017
Country/Territory	Turkey
City	Istanbul
Period	19/06/17 → 22/06/17

Bibliographical note

Publisher Copyright:
© 2017 IEEE.

Keywords

Eigenaxis rotations
Finite Time Attitude Control
Lyapunov Theory
Quaternion representation
Satellite Orientation

ASJC Scopus subject areas

Aerospace Engineering

Access to Document

10.1109/RAST.2017.8002933

Cite this

Amrr, S. M., Banerjee, A., Nabi, M., & Janardhanan, S. (2017). Finite time eigenaxis rotation using quaternion feedback. In M. F. Unal, A. Hacioglu, M. S. Yildiz, O. Altan, & M. Yorukoglu (Eds.), Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 (pp. 105-108). Article 8002933 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2017.8002933

Amrr, Syed Muhammad ; Banerjee, Arunava ; Nabi, M. et al. / Finite time eigenaxis rotation using quaternion feedback. Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017. editor / M.F. Unal ; A. Hacioglu ; M.S. Yildiz ; O. Altan ; M. Yorukoglu. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 105-108 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017).

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title = "Finite time eigenaxis rotation using quaternion feedback",

abstract = "The attitude of the spacecraft is its angular orientation in space. Attitude control design of a satellite system is an important area of space technology. An efficient controller is required to take the satellite system to its target orientation. In some cases, the maneuver need to be completed within a finite time. This paper introduces a novel control law which achieves finite time convergence to the required orientation. The control laws are shown to converge in a finite time for the satellite system by using Lyapunov theory and are also illustrated via simulation results.",

keywords = "Eigenaxis rotations, Finite Time Attitude Control, Lyapunov Theory, Quaternion representation, Satellite Orientation",

author = "Amrr, \{Syed Muhammad\} and Arunava Banerjee and M. Nabi and S. Janardhanan",

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year = "2017",

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Amrr, SM, Banerjee, A, Nabi, M & Janardhanan, S 2017, Finite time eigenaxis rotation using quaternion feedback. in MF Unal, A Hacioglu, MS Yildiz, O Altan & M Yorukoglu (eds), Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017., 8002933, Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Institute of Electrical and Electronics Engineers Inc., pp. 105-108, 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Istanbul, Turkey, 19/06/17. https://doi.org/10.1109/RAST.2017.8002933

Finite time eigenaxis rotation using quaternion feedback. / Amrr, Syed Muhammad; Banerjee, Arunava; Nabi, M. et al.
Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017. ed. / M.F. Unal; A. Hacioglu; M.S. Yildiz; O. Altan; M. Yorukoglu. Institute of Electrical and Electronics Engineers Inc., 2017. p. 105-108 8002933 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Janardhanan, S.

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AB - The attitude of the spacecraft is its angular orientation in space. Attitude control design of a satellite system is an important area of space technology. An efficient controller is required to take the satellite system to its target orientation. In some cases, the maneuver need to be completed within a finite time. This paper introduces a novel control law which achieves finite time convergence to the required orientation. The control laws are shown to converge in a finite time for the satellite system by using Lyapunov theory and are also illustrated via simulation results.

KW - Eigenaxis rotations

KW - Finite Time Attitude Control

KW - Lyapunov Theory

KW - Quaternion representation

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PB - Institute of Electrical and Electronics Engineers Inc.

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Amrr SM, Banerjee A, Nabi M, Janardhanan S. Finite time eigenaxis rotation using quaternion feedback. In Unal MF, Hacioglu A, Yildiz MS, Altan O, Yorukoglu M, editors, Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 105-108. 8002933. (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017). doi: 10.1109/RAST.2017.8002933

Finite time eigenaxis rotation using quaternion feedback

Abstract

Publication series

Conference

Bibliographical note

Keywords

ASJC Scopus subject areas

Access to Document

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Cite this