Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating
With the demand for high resolution remote sensing, load array technology has gradually become an effective measure to improve imaging resolution. However, the external flow and internal engine vibration disturbance may lead to the flexible deformation of wings. The traditional rigid baseline error...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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MDPI AG
2020-04-01
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| Series: | Sensors |
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| Online Access: | https://www.mdpi.com/1424-8220/20/7/2120 |
| _version_ | 1827719041804926976 |
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| author | Wen Ye Bin Gu Yun Wang |
| author_facet | Wen Ye Bin Gu Yun Wang |
| author_sort | Wen Ye |
| collection | DOAJ |
| description | With the demand for high resolution remote sensing, load array technology has gradually become an effective measure to improve imaging resolution. However, the external flow and internal engine vibration disturbance may lead to the flexible deformation of wings. The traditional rigid baseline error compensation method cannot solve the problem of serious coupling movement error caused by flexible deformation. To address the problem, a transfer alignment model based on fiber Bragg grating for distributed position and orientation system is proposed in this paper. Firstly, based on the multidimensional requirements of flexible deformation information, the layout scheme of fiber Bragg grating was designed, then the continuous strain in the wing surface was obtained after the quadratic fitting of strain measured by fiber Bragg gratings, and the deformation displacement and angle are calculated. Thirdly, flexible deformation compensation for distributed position and orientation system based on fiber Bragg grating was studied. The state equation including position error, velocity error, misalignment angle, and inertial device error was established. The position and attitude information compensated by the flexible lever arm was used as the quantitative measurement. The filtering estimation improved the measurement accuracy of the slave inertial navigation systems. At last, the experiment was carried out and showed that the accuracy of the transfer alignment has been improved significantly. |
| first_indexed | 2024-03-10T20:34:44Z |
| format | Article |
| id | doaj.art-8113eaaea0f54d4c984174247884ab9c |
| institution | Directory Open Access Journal |
| issn | 1424-8220 |
| language | English |
| last_indexed | 2024-03-10T20:34:44Z |
| publishDate | 2020-04-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Sensors |
| spelling | doaj.art-8113eaaea0f54d4c984174247884ab9c2023-11-19T21:07:47ZengMDPI AGSensors1424-82202020-04-01207212010.3390/s20072120Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg GratingWen Ye0Bin Gu1Yun Wang2Division of Mechanics and Acoustic Metrology, National Institute of Metrology, Beijing 100029, ChinaChina Academy of Electronics and Information Technology, Beijing 100041, ChinaProspective Technology Research Department, SAIC Group, Shanghai 200041, ChinaWith the demand for high resolution remote sensing, load array technology has gradually become an effective measure to improve imaging resolution. However, the external flow and internal engine vibration disturbance may lead to the flexible deformation of wings. The traditional rigid baseline error compensation method cannot solve the problem of serious coupling movement error caused by flexible deformation. To address the problem, a transfer alignment model based on fiber Bragg grating for distributed position and orientation system is proposed in this paper. Firstly, based on the multidimensional requirements of flexible deformation information, the layout scheme of fiber Bragg grating was designed, then the continuous strain in the wing surface was obtained after the quadratic fitting of strain measured by fiber Bragg gratings, and the deformation displacement and angle are calculated. Thirdly, flexible deformation compensation for distributed position and orientation system based on fiber Bragg grating was studied. The state equation including position error, velocity error, misalignment angle, and inertial device error was established. The position and attitude information compensated by the flexible lever arm was used as the quantitative measurement. The filtering estimation improved the measurement accuracy of the slave inertial navigation systems. At last, the experiment was carried out and showed that the accuracy of the transfer alignment has been improved significantly.https://www.mdpi.com/1424-8220/20/7/2120distributed position and orientation systemtransfer alignmentfiber bragg gratingwing deformation measurement |
| spellingShingle | Wen Ye Bin Gu Yun Wang Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating Sensors distributed position and orientation system transfer alignment fiber bragg grating wing deformation measurement |
| title | Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating |
| title_full | Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating |
| title_fullStr | Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating |
| title_full_unstemmed | Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating |
| title_short | Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating |
| title_sort | airborne distributed position and orientation system transfer alignment method based on fiber bragg grating |
| topic | distributed position and orientation system transfer alignment fiber bragg grating wing deformation measurement |
| url | https://www.mdpi.com/1424-8220/20/7/2120 |
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