Abstract
Due to the observations of out small disturbance in spacecraft, a promising new field of research in inertial attitude sensor has been developed. However, exploration of new spacecraft under high-frequency oscillation has been hampered by the lack of a portable, reliable and highly sensitive broadband sensor. In this paper, the laboratory tests of a broadband inertial attitude sensor named micro-vibration measurement sensor (MMS) in spacecraft based on interferometric fiber optic gyroscope (IFOG) is firstly reported. The noise level by operating range diagrams and Allan deviation is estimated and tests of the sensors, which are demonstrated the reliability of MMS in filed installations. This new technology presents a wide range of field applications in spacecraft, earthquake engineering and seismology.
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This work was supported by a project numbered 41417060102.
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Yang, B. et al. (2022). Development of Broadband Sensors Based on Fiber Optic Gyroscope. In: Jain, L.C., Kountchev, R., Hu, B., Kountcheva, R. (eds) Smart Communications, Intelligent Algorithms and Interactive Methods. Smart Innovation, Systems and Technologies, vol 257. Springer, Singapore. https://doi.org/10.1007/978-981-16-5164-9_28
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DOI: https://doi.org/10.1007/978-981-16-5164-9_28
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