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Improving Strapdown Inertial Navigation System Performance by Self-Compensation of Inertial Sensor Errors Cover

Improving Strapdown Inertial Navigation System Performance by Self-Compensation of Inertial Sensor Errors

Open Access
|Dec 2023

Figures & Tables

Figure 1.

Scheme of the IMU on a rotating platform. XBYBZB – the body frame; XSYSZS – the sensor frame. IMU, inertial measurement unit.
Scheme of the IMU on a rotating platform. XBYBZB – the body frame; XSYSZS – the sensor frame. IMU, inertial measurement unit.

Figure 2.

Scheme of the stand of static products (A). uniaxial rotary stand MPU-1 (B) and a test sample, installed on it in a position with a horizontal axis of rotation (C).
Scheme of the stand of static products (A). uniaxial rotary stand MPU-1 (B) and a test sample, installed on it in a position with a horizontal axis of rotation (C).

Figure 3.

IMU output without modulating rotation. IMU, inertial measurement unit.
IMU output without modulating rotation. IMU, inertial measurement unit.

Figure 4.

Output signals of rotated IMU with modulating rotation along a vertical axis. IMU, inertial measurement unit.
Output signals of rotated IMU with modulating rotation along a vertical axis. IMU, inertial measurement unit.

Figure 5.

Output signals of rotated IMU with modulating rotation along a horizontal axis. IMU, inertial measurement unit.
Output signals of rotated IMU with modulating rotation along a horizontal axis. IMU, inertial measurement unit.

Figure 6.

Graphs of the estimations (3) of the RM IMU with vertical and horizontal rotation axis compared with the stationary case. IMU, inertial measurement unit; RM, rotation modulation.
Graphs of the estimations (3) of the RM IMU with vertical and horizontal rotation axis compared with the stationary case. IMU, inertial measurement unit; RM, rotation modulation.

Results of static experiments_

StaticRM (vertical axis)RM (horizontal axis)
ε(t = 300s ),[deg]X16.35–0.951.08
Y–53.110.90.86
Z5.6214.079.2
ΔV (t = 300s ),[m/s]X415.37–33.6630.83
Y–332.515.6232.96
Z137.2695.76117.3
ΔS (t = 300s ),[km]X41.46–3.753.3
Y–33.294.26.08
Z6.678.7923.16

Characteristics of IMU Xsens MTI-1 sensors_

Accelometr blockGyroscope block
Measurement range±16 g±2,000°/s
Zero offset instability0.03 mg10°/h
Bandwidth (–3 dB)324 (Z: 262) Hz255 Hz
Noise density120μg/√Hz0.007°/s/√Hz
Non-linearity0.5%FS0.1%FS
Language: English
Page range: 41 - 51
Submitted on: Aug 1, 2023
Accepted on: Oct 26, 2023
Published on: Dec 8, 2023
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2023 Mykola Chernyak, Vadym Kolesnyk, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.