2019
DOI: 10.1134/s2075108719040023
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Comparative Analysis of Fusion Algorithms in a Loosely-Coupled Integrated Navigation System on the Basis of Real Data Processing

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Cited by 18 publications
(8 citation statements)
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“…where C n b is the rotation matrix from the body frame (b-frame, Forward-Right-Down) to the navigation frame (n-frame, North-East-Down); f b is the specific force in the b-frame; ω n ie is the angular rate of the earth frame (e-frame) relative to the inertial frame (i-frame) in the n-frame; ω n en is the angular rate of the n-frame relative to the e-frame in the n-frame; v n is the velocity in the n-frame; g n l is the normal gravity in the local position in the n-frame; C e n is the rotation matrix from the n-frame to the e-frame, which represent the geodetic latitude and longitude; h and v D are the ellipsoid height and velocity in the down direction, respectively; ω b ib is the angular rate of the b-frame relative to the i-frame in the b-frame; ω n in is the angular rate of the n-frame relative to the i-frame in the n-frame; (×) is skew symmetric matrix. According to Equation (3), the unsimplified INS speed update can be written as follows: (7) where…”
Section: Ins Dynamic Modelmentioning
confidence: 99%
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“…where C n b is the rotation matrix from the body frame (b-frame, Forward-Right-Down) to the navigation frame (n-frame, North-East-Down); f b is the specific force in the b-frame; ω n ie is the angular rate of the earth frame (e-frame) relative to the inertial frame (i-frame) in the n-frame; ω n en is the angular rate of the n-frame relative to the e-frame in the n-frame; v n is the velocity in the n-frame; g n l is the normal gravity in the local position in the n-frame; C e n is the rotation matrix from the n-frame to the e-frame, which represent the geodetic latitude and longitude; h and v D are the ellipsoid height and velocity in the down direction, respectively; ω b ib is the angular rate of the b-frame relative to the i-frame in the b-frame; ω n in is the angular rate of the n-frame relative to the i-frame in the n-frame; (×) is skew symmetric matrix. According to Equation (3), the unsimplified INS speed update can be written as follows: (7) where…”
Section: Ins Dynamic Modelmentioning
confidence: 99%
“…GNSS and INS have strong complementarity with each other in many aspects such as error characteristics. Combining GNSS and INS can provide more accurate, continuous, and reliable navigation information (including position, velocity, and attitude) than individual GNSS or INS [6,7].…”
Section: Introductionmentioning
confidence: 99%
“…. The continuous Markov process described by (27) can be discretised with step Δt and the following random sequence can be obtained…”
Section: Parameter Identification Of First-order Markov Processmentioning
confidence: 99%
“…The solution of the estimation problem can also be simplified by searching for estimates within some limited class, for example, the class of linear estimates [23,24]. Among other procedures used in this field, we should mention unscented transformation (Unscented KF, UKF) [25][26][27] and cubature formulas [28].…”
Section: Introductionmentioning
confidence: 99%
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