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2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) 2018
DOI: 10.23919/icins.2018.8405845
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On integration of a strapdown inertial navigation system with modern magnetic sensors

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Cited by 8 publications
(4 citation statements)
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“…A Kalman filter with magnetic field observations is presented to correct the cumulative error of the inertial navigation [21]. The difference between the geomagnetic model value and the measured magnetic field value is taken as an observation of the Kalman filter.…”
Section: Related Workmentioning
confidence: 99%
“…A Kalman filter with magnetic field observations is presented to correct the cumulative error of the inertial navigation [21]. The difference between the geomagnetic model value and the measured magnetic field value is taken as an observation of the Kalman filter.…”
Section: Related Workmentioning
confidence: 99%
“…Algorithm 3 (as main part of algorithm of calculations of Rodrigues-Hamilton parameters) is realized [8, p. 316] in the laser aviation strapdown inertial navigation system SINS-85, serially [9] produced since 2002 and intended for the use on the airplanes Il-96-300, Tu-204, Тu-334. Modifications of the system SINS-85 (SINS-77, SINS-Т, SINS SP-1, SINS SP-2) are used on the airplanes .…”
Section: A Application Of Nonclassical Quaternions For Determination ...mentioning
confidence: 99%
“…The measurement error of Inertial Navigation System (INS) accumulates with time, so INS needs to be corrected periodically by other auxiliary methods. An effective method is to integrate geomagnetic navigation and inertial navigation [1,2]. Many scientists around the world are studying geomagnetic navigation.…”
Section: Introductionmentioning
confidence: 99%