The paper is dedicated to the 100th anniversary of the birth of V.I. Kuznetsov and A.Yu. Ishlinskii, Academicians of the Academy of Sciences of the USSR, to the 100th anniversary of Sagnac experiment, and to the 50th anniversary of laser gyroscopy
Abstract
Accurate error equations for strapdown interial navigation system (SINS) are derived partly with account of nonideal onboard time scale. Comments are given on specific features of SINS behaviour unnoticed earlier using approximate equations of INS errors. Error equations are first proposed to improve SINS accuracy as well as to analyze it. Limits on SINS accuracy due to quantum noise of Sagnac effect gyros such as laser and fiber-optic gyros and atom interferometers on de Broiglie waves [1] are estimated.
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Final report on the research Issledovanie vozmozhnostei i putei sozdaniya printsipial’no novykh tipov vysokopretsizionnykh giroskopov na obobshchennom effekte San’yaka (na volnakh de Broilya, Bose-Einshtein kondensatakh i sverkhtekuchesti geliya) i mikromekhanicheskikh giroskopov povyshennoi tochnosti s raznesennymi chastotami vozbuzhdeniya i s’ema dlya upravleniya dvizheniem kosmicheskikh apparatov (Studying the Feasibility and Methods of Creating Principally New High Precision Gyros Based on General Sagnac Effect (de Broiglie Waves, Bose-Einstein Condensates and Helium Superfluidity) and MEMS Gyros of Enhanced Accuracy with Spaced Drive and Sense Frequencies for Spacecraft Motion Control), Principal investigator N.I. Krobka, Federal State Unitary Enterprise Center for Ground-Based Space Infrastructure, Kuznetsov Scientific Research Institute of Applied Mechanics, vols. 1–7, 2012.
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Published in Giroskopiya i Navigatsiya, 2013, No. 4, pp. 46–59.
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Krobka, N.I. Estimating quantum limits on SINS accuracy based on accurate error equations. Gyroscopy Navig. 5, 9–19 (2014). https://doi.org/10.1134/S2075108714010064
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DOI: https://doi.org/10.1134/S2075108714010064