Issue #8/2021
P. Novikov
IMPROVING THE ACCURACY OF ORIENTATION ANGLES DETECTION AT STRAPDOWN INERTIAL NAVIGATION SYSTEM
IMPROVING THE ACCURACY OF ORIENTATION ANGLES DETECTION AT STRAPDOWN INERTIAL NAVIGATION SYSTEM
DOI: 10.22184/1992-4178.2021.209.8.152.155
The article considers the method of SINS correction using the Kalman filter algorithm, the measurement vector of which is formed on the basis of the readings of the satellite navigation system (SNS) receiver. The method is simple to implement and improves the accuracy of the navigation solution.
The article considers the method of SINS correction using the Kalman filter algorithm, the measurement vector of which is formed on the basis of the readings of the satellite navigation system (SNS) receiver. The method is simple to implement and improves the accuracy of the navigation solution.
Теги: kalman filter output accuracy strapdown inertial navigation system (sins) бесплатформенная инерциальная навигационная система (бинс) точность выходных показаний фильтр калмана
IMPROVING THE ACCURACY OF ORIENTATION ANGLES DETECTION AT STRAPDOWN INERTIAL NAVIGATION SYSTEM
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