Paper
17 October 2012 Fiber optic gyros in a high-performance, high-reliability inertial reference unit for commercial satellites
S. Sanders, A. Taranta, S. Mosor, M. Alden, L. Hendry, R. DeMaio, N. Giere, J. Sewell
Author Affiliations +
Proceedings Volume 8421, OFS2012 22nd International Conference on Optical Fiber Sensors; 842106 (2012) https://doi.org/10.1117/12.975535
Event: OFS2012 22nd International Conference on Optical Fiber Sensor, 2012, Beijing, China
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.
© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
S. Sanders, A. Taranta, S. Mosor, M. Alden, L. Hendry, R. DeMaio, N. Giere, and J. Sewell "Fiber optic gyros in a high-performance, high-reliability inertial reference unit for commercial satellites", Proc. SPIE 8421, OFS2012 22nd International Conference on Optical Fiber Sensors, 842106 (17 October 2012); https://doi.org/10.1117/12.975535
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Cited by 4 scholarly publications.
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KEYWORDS
Gyroscopes

Fiber optic gyroscopes

Satellites

Satellite communications

Head

Sensors

Humidity

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