Research on Relative Position Testing Based on Inertial Navigation and Ultra-Wideband Fusion System

Aiming at the challenge that the direction of cable force is difficult to be measured directly in helicopter flight test with slung-load, the inertial navigation and ultra-wideband integration method is used to measure the relative position of slung-load and body, so the direction can be measured indirectly. This paper studies the technology of improving the positioning accuracy of fusion system from three aspects: time registration, base station layout and anti-interference. The results indicate that the label positioning accuracy is higher when the base station is arranged in a circular pattern; by designing registers and using the least squares method, time alignment of the two data sources in the fusion system can be achieved; inertial navigation data correction of ultra-wideband data can improve its positioning accuracy. Experimental data shows that the accuracy of the fusion system can meet the requirements for testing the relative position of the slung-load.

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Published
2024-10-25
DOI
https://doi.org/10.1109/isstc63573.2024.10824212
Primary Topic
Inertial Sensor and Navigation
Type
article
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article

Research on Relative Position Testing Based on Inertial Navigation and Ultra-Wideband Fusion System

Wei Yuan, Chuan Yin
Inertial Sensor and Navigation
article

Research on Relative Position Testing Based on Inertial Navigation and Ultra-Wideband Fusion System

Wei Yuan, Chuan Yin
article en

Abstract

Aiming at the challenge that the direction of cable force is difficult to be measured directly in helicopter flight test with slung-load, the inertial navigation and ultra-wideband integration method is used to measure the relative position of slung-load and body, so the direction can be measured indirectly. This paper studies the technology of improving the positioning accuracy of fusion system from three aspects: time registration, base station layout and anti-interference. The results indicate that the label positioning accuracy is higher when the base station is arranged in a circular pattern; by designing registers and using the least squares method, time alignment of the two data sources in the fusion system can be achieved; inertial navigation data correction of ultra-wideband data can improve its positioning accuracy. Experimental data shows that the accuracy of the fusion system can meet the requirements for testing the relative position of the slung-load.

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Inertial Sensor and Navigation
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