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Featured researches published by Wei Quan.


AOPC 2015: Advances in Laser Technology and Applications | 2015

Design and realization of beam collimation system for semiconductor laser in atomic magnetometer

Xi Chen; Wei Quan; Lihong Duan; Baiqi Liu; Fan Xu

Atomic magnetometer which uses alkali atoms as the sensors can realize ultrahigh sensitivity magnetic field measurement and has extensive applications scientific researches. Semiconductor lasers are used as the pump and probe laser in atomic magnetometer. Due to structural characteristics of semiconductor laser, beam divergence angles in vertical and horizontal direction have large deviation and laser beam diverges extremely fast. However, poor laser beam affects the implementation of atomic magnetometer sensitivity adversely. Only the circular laser beam with Gaussian distribution guarantees the homogeneous polarization of alkali atom vapor and high efficiency of atomic magnetometer. Consequently, a beam collimation system must be designed. In this paper, a collimation method using a thin lens and a pair of anamorphic prisms is proposed to guarantee the laser spot size approximately constant. The thin lens is used to decrease fast-axis divergence angle and ensure transmitted light is parallel. The anamorphic prisms pairs expand the laser beam in slow-axis and make the beam spot nearly round. Initially, the effect of thin lenses and anamorphic prisms on the relationship of input and output beam profiles is theoretically analyzed based on principle of geometrical optics. Then the software Zemax is used to simulate the collimation system. Finally, a beam collimation system is designed and tested. The experiment result shows that the laser beam size is approximately 2×2cm2 and the beam approximate a Gaussian profile, which can meet the requirement of the atomic magnetometer.


Archive | 2008

Integrated navigation computer based on DSP and FPGA

Jiancheng Fang; Jintao Li; Wei Quan; Fan Xu


Archive | 2007

On-line calibration method for shield machine automatic guiding system based on optical fiber gyro and PSD laser target

Baiqi Liu; Jiancheng Fang; Wei Quan; Zhaohua Yang; Sheng Yang; Jintao Li


Archive | 2007

Method of realizing combined navigation system structure for aviation

Jiancheng Fang; Fan Xu; Wei Sheng; Peiling Cui; Baiqi Liu; Wei Quan


Archive | 2007

Shield machine automatic guiding system based on optical fiber gyro and PSD laser target

Jiancheng Fang; Baiqi Liu; Sheng Yang; Jintao Li; Zhaohua Yang; Wei Quan


Archive | 2011

Satellite attitude control semiphysical simulation system based on multi-target machine

Lei Guo; Jianzhong Qiao; Bin Ouyang; Yuanjin Yu; Cuicui Liu; Hua Liu; Zhaohua Yang; Wei Quan; Peiling Cui; Chao Han


Archive | 2007

High precision low cost starlight simulator

Jiancheng Fang; Wei Quan; Fan Wu; Baiqi Liu; Sheng Yang


Archive | 2007

Integrated combined navigation computer based on double DSP

Jiancheng Fang; Sheng Yang; Baiqi Liu; Yu Zhang; Wei Quan; Fan Xu


Archive | 2012

Micro-satellite attitude determination method based on ESOQPF (estimar of quaternion particle filter ) and UKF (unscented kalman filter) master-slave filtering

Peiling Cui; Huijuan Zhang; Wei Quan; Jiancheng Fang; Lei Guo


Archive | 2011

Integrated attitude determination method based on ant colony unscented particle filter algorithm

Wei Quan; Lei Guo; Jiancheng Fang; Cuicui Liu; Zhaohua Yang; Peiling Cui

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Baiqi Liu

China Aerospace Science and Technology Corporation

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Fan Xu

China Aerospace Science and Technology Corporation

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