Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating
Airborne Distributed Position and Orientation System Transfer Alignment Method Based on Fiber Bragg Grating
复制标题
基于光纤布拉格光栅的机载分布式位置定向系统传递对准方法
DOI:
10.3390/s20072120
复制
发表时间:
2020-04-01
期刊:
影响因子:
3.9
通讯作者:
Wang, Yun
中科院分区:
文献类型:
--
作者:
Ye, Wen;Gu, Bin;Wang, Yun
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.