Aiming at the problem of incomplete parameter identification for error calibration in hybrid
inertial navigation systems (HINS), which leads to poor navigation accuracy. The article …

In a high-precision ring laser gyro (RLG) inertial navigation system (INS), the g-sensitive
misalignment caused by external acceleration represents one of the main error sources …

The autonomous navigation technology of INS has always attracted the attention of many
scholars. In satellite-denied environment, making full use of the auxiliary sensors with …

Dual-axis rotational inertial navigation system (DRINS) can achieve self-calibration of error
parameters through a reasonable rotation scheme. However, the traditional self-calibration …

In this article, the attitude of the master inertial navigation system (INS) installed on the
autonomous drone launcher and the slave INS installed on the autonomous drone are …

Strapdown inertial navigation system/celestial navigation system (SINS/CNS) integrated
navigation with narrow-field-of-view (NFOV) star tracker is widely employed in the aviation …

Dual-axis rotational inertial navigation systems (RINSs) can be categorized into inner-
azimuth RINSs and outer-azimuth RINSs based on different frame structures. Previous …

The problem of poor initial alignment anti-interference ability of the vehicle-mounted single-
axis rotating inertial navigation system in complex environments leading to poor navigation …

A vehicle integrated navigation system based on Global Navigation Satellite System (GNSS)
aided Inertial Navigation System (INS) enhances its navigation accuracy by utilizing non …

The Kalman filter method plays a crucial role in enhancing the navigation accuracy of the
dual-axis rotational inertial navigation system (RINS) through periodic estimation and …