2023
DOI: 10.3390/s23063091
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A Combination Scheme of Pure Strapdown and Dual-Axis Rotation Inertial Navigation Systems

Abstract: Compared with the strapdown inertial navigation system (SINS), the rotation strapdown inertial navigation system (RSINS) can effectively improve the accuracy of navigation information, but rotational modulation also leads to an increase in the oscillation frequency of attitude errors. In this paper, a dual-inertial navigation scheme that combines the strapdown inertial navigation system and the dual-axis rotation inertial navigation system is proposed, which can effectively improve the attitude error accuracy … Show more

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Cited by 3 publications
(1 citation statement)
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“…The strap-down inertial navigation error propagation equation is used to build the system state model [19], and the difference between the geomagnetic intensity of the inertial navigation indication position and the actual measured geomagnetic intensity is used as the observation measurement to build the integrated navigation nonlinear system model; adopting an improved unscented Kalman filtering method to implement estimation and correction, in order to achieve the design of an inertial/geomagnetic tight integrated navigation system and improve system accuracy and reliability. The diagram of the inertial/geomagnetic tight integrated navigation system is shown in figure 1.…”
Section: Establishment Of State Vector and State Equationmentioning
confidence: 99%
“…The strap-down inertial navigation error propagation equation is used to build the system state model [19], and the difference between the geomagnetic intensity of the inertial navigation indication position and the actual measured geomagnetic intensity is used as the observation measurement to build the integrated navigation nonlinear system model; adopting an improved unscented Kalman filtering method to implement estimation and correction, in order to achieve the design of an inertial/geomagnetic tight integrated navigation system and improve system accuracy and reliability. The diagram of the inertial/geomagnetic tight integrated navigation system is shown in figure 1.…”
Section: Establishment Of State Vector and State Equationmentioning
confidence: 99%