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Fiber optic gyros in a high-performance, high-reliability inertial reference unit for commercial satellites

Fiber optic gyros in a high-performance, high-reliability inertial reference unit for commercial satellites
Fiber optic gyros in a high-performance, high-reliability inertial reference unit for commercial satellites
Honeywell Space Systems Division has successfully completed development of the Interferometric Fiber Optic Gyroscopes (IFOG) for a next-generation Inertial Reference Unit (IRU) to point commercial satellites. The design, build, and test phase of an engineering-model of this IRU, nicknamed Spirit, completed in 2011. The Spirit IRU complements the existing portfolio of Honeywell navigation products, such as the Miniature Inertial Measurement Unit (MIMU), by leveraging the long life and excellent performance inherent in FOG technology. This paper provides an overview of the Spirit system along with initial results from gyro performance and life testing.
0277-786X
SPIE - The International Society for Optical Engineering
Sanders, S.
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Taranta, A.
bc2e834f-0d85-44a1-a874-8150df1f73d9
Mosor, S.
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Alden, M.
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Hendry, L.
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DeMaio, R.
c4714d39-19f6-4745-a0ca-b14212f5ab64
Giere, N.
eca28d13-785f-40ff-b01a-24c6e72c7ff6
Sewell, J.
a84714e3-c945-4e9b-bbe4-f6a8680cfce7
et al.
Sanders, S.
3d6fa934-58ed-49e4-920d-a9c16bf403bd
Taranta, A.
bc2e834f-0d85-44a1-a874-8150df1f73d9
Mosor, S.
a31b196a-6cfb-40b5-9a58-88aee26a34c6
Alden, M.
8a629051-086d-4878-833b-54b88a111a65
Hendry, L.
71933493-16ec-47b7-a367-fffb7888a517
DeMaio, R.
c4714d39-19f6-4745-a0ca-b14212f5ab64
Giere, N.
eca28d13-785f-40ff-b01a-24c6e72c7ff6
Sewell, J.
a84714e3-c945-4e9b-bbe4-f6a8680cfce7

Sanders, S., Taranta, A. and Alden, M. , et al. (2012) Fiber optic gyros in a high-performance, high-reliability inertial reference unit for commercial satellites. In 22nd International Conference on Optical Fiber Sensors. vol. 8421, SPIE - The International Society for Optical Engineering.. (doi:10.1117/12.975535).

Record type: Conference or Workshop Item (Paper)

Abstract

Honeywell Space Systems Division has successfully completed development of the Interferometric Fiber Optic Gyroscopes (IFOG) for a next-generation Inertial Reference Unit (IRU) to point commercial satellites. The design, build, and test phase of an engineering-model of this IRU, nicknamed Spirit, completed in 2011. The Spirit IRU complements the existing portfolio of Honeywell navigation products, such as the Miniature Inertial Measurement Unit (MIMU), by leveraging the long life and excellent performance inherent in FOG technology. This paper provides an overview of the Spirit system along with initial results from gyro performance and life testing.

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More information

Published date: 2012
Additional Information: © (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Venue - Dates: 22nd International Conference on Optical Fiber Sensors, , Beijing, China, 2012-10-15 - 2012-10-19

Identifiers

Local EPrints ID: 475764
URI: http://eprints.soton.ac.uk/id/eprint/475764
ISSN: 0277-786X
PURE UUID: 93e4d510-0c96-4d5c-86c7-eaccd6d27fe5
ORCID for A. Taranta: ORCID iD orcid.org/0000-0002-5666-6800

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Date deposited: 28 Mar 2023 16:30
Last modified: 17 Mar 2024 03:40

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Contributors

Author: S. Sanders
Author: A. Taranta ORCID iD
Author: S. Mosor
Author: M. Alden
Author: L. Hendry
Author: R. DeMaio
Author: N. Giere
Author: J. Sewell
Corporate Author: et al.

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