2022
DOI: 10.1088/1361-6501/aca421
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An improved GNSS/INS navigation method based on cubature Kalman filter for occluded environment

Abstract: GNSS/INS (Global Navigation Satellite System and Inertial Navigation System) based on CKF (Cubature Kalman Filter) can provide an effective land vehicle navigation and positioning solution. The accuracy of CKF depends mainly on the prior Probability Density Function (PDF), which is inaccurate when the GNSS signal is temporarily blocked in an urban environment. Although the ICKF (Improved Cubature Kalman Filter) can reduce cubature point errors by using the historical information obtained iteratively, the gener… Show more

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Cited by 10 publications
(8 citation statements)
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“…In comparison to the Unscented Kalman filter algorithm, the Cubature Kalman Filter algorithm obtains the volume points by calculating the spheri-cal radial volume criterion without linearizing the state equation directly transferring the volume points by the nonlinear state equation while ensuring that the weights are always positive. This improves the algorithm's robustness and accuracy [22][23][24].…”
Section: Target Localization Methods Based On Cubature Kalman Filtermentioning
confidence: 99%
“…In comparison to the Unscented Kalman filter algorithm, the Cubature Kalman Filter algorithm obtains the volume points by calculating the spheri-cal radial volume criterion without linearizing the state equation directly transferring the volume points by the nonlinear state equation while ensuring that the weights are always positive. This improves the algorithm's robustness and accuracy [22][23][24].…”
Section: Target Localization Methods Based On Cubature Kalman Filtermentioning
confidence: 99%
“…This approach contributes to enhancing the precision of the entire navigation system. When passing through a tunnel, although the signal is blocked and the information is inaccurate, the attitude information in the TMR digital compass is accurate and can continue to provide attitude correction for the [ 35 , 36 , 37 , 38 , 39 , 40 , 41 , 42 , 43 , 44 , 45 , 46 , 47 , 48 , 49 , 50 , 51 , 52 , 53 , 54 , 55 , 56 , 57 , 58 , 59 , 60 , 61 , 62 , 63 ].…”
Section: Design Of High-precision Portable Digital Compass Systemmentioning
confidence: 99%
“…This paper defines the inertial coordinate frame as the I-frame, the carrier coordinate frame as the b-frame, and the navigation coordinate frame as the n-frame, which has east, north, and up directions and follows the right-hand rule [24]. The error equation of attitude change with time can be obtained as shown in equation (5).…”
Section: Error Analysis Of Inertial Navigation Systemsmentioning
confidence: 99%
“…The first idea is to estimate and compensate for the modeling error and utilize various methods to approximate the real model of the system error to improve the accuracy of the integrated navigation. Examples of such approaches include adding external sensors [3], using motion constraint algorithms [4], and improving Kalman filtering algorithms [5]. The second approach involves using artificial intelligence to establish the relationship between the vehicle dynamics and the INS error for the part of the system that is nonlinear or difficult to model, and to predict the future vehicle trajectory.…”
Section: Introductionmentioning
confidence: 99%