Radiation-Induced Magneto-Optic Fluctuations in Spaceborne Fiber-Optic Gyroscope

Wang, Xiaowei; Song, Ningfang; Jin, Jing; Zhang, Zuchen; Wang, Tingting; Song, Jingming

doi:10.1109/jlt.2022.3216485

Cited by 3 publications

(1 citation statement)

References 35 publications

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“…The location (course) of an object in the inertial coordinate system (CS): its speed, acceleration and other parameters necessary to control the movement and determine its location in space are really important. To obtain information about the movement of an object, its INS, first of all, includes: gyroscopes for determining the angles of inclination of the main axes in the inertial CS and accelerometers for determining linear accelerations [3][4][5][6] . Depending on the design of a closed optical loop (interferometer), optical gyroscope (OG) are divided into ring laser gyroscopes (RLG), fiber optical gyroscopes (FOG) of the interferometric type (IFOG -Interferometric Fiber Optic Gyroscope) and FOG with a passive resonator (RFOG − Resonant Fiber Optic Gyroscope).…”

Section: Introductionmentioning

confidence: 99%

Fiber-optic system for control of the orientation of objects in space

Hnatenko,

Machekhin,

Bilichenko

et al. 2023

Optical Fibers and Their Applications 2023

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This article illustrates a system for stabilizing objects in space based on integral fiber elements. The proposed system showed results commensurate with similar systems with a length of tens of kilometers of SMF-28 optical fiber, while using PANDA type optical fiber is only 200 m. In the work, a model of the system was developed and experimental studies of the response and angular velocity of the gyroscope were carried out.

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Section: Introductionmentioning

confidence: 99%