For rotational inertial navigation system (RINS), the system error can be compensated by
rotating the inertial measurement unit (IMU) with one or more axis regularly, and the error …

An eight-position self-calibration method for a dual-axis rotational Inertial Navigation System
(INS) is provided in this paper. By experiencing two more positions with tilt attitudes than …

Rotational inertial navigation system (RINS) could improve navigation performance by
rotating the inertial measurement unit (IMU) with gimbals, and error parameters could be self …

Rotational inertial navigation system (RINS) could improve the navigation performance by
rotating the IMU around gimbals, and the structure and function of the dual-axis RINS also …

Navigation accuracy of the inertial navigation system (INS) could be greatly improved by
rotating the inertial measurement unit around gimbals. However, the attitude output accuracy …

The navigation performance of the rotational inertial navigation system (RINS) could be
greatly improved by rotating the inertial measurement unit with gimbals, and self-calibration …

Gravity-matching algorithm is a key to the gravity-aided inertial navigation system (INS). The
traditional particle filter-based matching algorithm with a gravity sample vector is efficient …

A spherical motor has multiple degrees of freedom. Its motion control requires an accurate
attitude detection system. This study proposes a low‐cost microelectromechanical system …

In the rotational inertial navigation system (RINS), the rotation scheme affects the system's
performance directly. Improper rotation scheme may excite devices' errors instead of …

Rotation modulation is an effective method to enhance the accuracy of an inertial navigation
system (INS) by modulating the gyroscope drifts and accelerometer bias errors into …