G
Glen A. Sanders
Researcher at Honeywell
Publications - 178
Citations - 2093
Glen A. Sanders is an academic researcher from Honeywell. The author has contributed to research in topics: Resonator & Optical fiber. The author has an hindex of 23, co-authored 178 publications receiving 1987 citations.
Papers
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Proceedings ArticleDOI
Fiber optic gyro development at Honeywell
Glen A. Sanders,Steven J. Sanders,Lee K. Strandjord,Tiequn Qiu,Jianfeng Wu,Marc Smiciklas,Derek Mead,Sorin Mosor,Alejo Arrizon,Waymon Ho,Mary K. Salit +10 more
TL;DR: In this article, two major architectures of fiber optic gyroscopes have been under development at Honeywell in recent years, including the interferometric fiber-optic gyroscope (IFOG) and the resonator-fiber optic gyro (RFOG).
Journal ArticleDOI
Theory of polarization evolution in interferometric fiber-optic depolarized gyros
TL;DR: In this article, a relatively comprehensive analysis of polarization evolution in depolarized interferometric fiber-optic gyroscopes is presented, together with signal fading and mean wavelength stability.
Patent
System and method for stabilizing light sources in resonator gyro
TL;DR: In this paper, a method and apparatus for stabilizing laser light sources of a resonator gyro is described, and a controller coupled to the resonance detection circuit and the first and second light sources is presented.
Proceedings ArticleDOI
Hollow Core Fiber Optic Ring Resonator for Rotation Sensing
TL;DR: In this article, an exciting new fiber optic resonator architecture that addresses performance barriers of the past is presented for applications in rotation sensing, which uses bandgap fiber and shows encouraging performance.
Proceedings ArticleDOI
Fiber optic gyros for space, marine, and aviation applications
Glen A. Sanders,Bogdan Szafraniec,Ren-Young Liu,Clarence L. Laskoskie,Lee K. Strandjord,George A. Weed +5 more
TL;DR: Fiber-optic gyroscopes under development at Honeywell as the primary next generation inertial sensor have been successfully transitioned to production for attitude heading reference systems and the results of this effort are reported.