[1].Wang Lei, Li Kui, Liu Zengjun, et al. Rapid detection of index for encoder in rotary inertial navigation system. Optics Express, 2016, 24(5):5591; doi:10.1364/OE.24.005591
[2].Wang Lei, Wang Wei, Zhang Qian, et al.Self-calibration method based on navigation in high-precision inertial navigation system with fiber optic gyro. Optical Engineering, 2014, 53(6):064103; doi:10.1117/1.OE.53.6.064103
[3].Sui Jie, Wang Lei*, Wang Wei, et al. Improvement on the Pitch and Roll Output of Rotation Inertial Navigation System. IEEE Sensors Journal, 2017, PP(99):1-1; doi:10.1109/JSEN.2017.2691717
[4].Liu Zengjun, Wang Lei*, Li Kui, et al. An Improved Rotation Scheme for Dual-Axis Rotational Inertial Navigation System. IEEE Sensors Journal, 2017, 17(13):4189-4196; doi:10.1109/JSEN.2017.2703604
[5].Zhang Qian, Wang Lei*, Liu Zengjun, et al. Innovative self-calibration method for accelerometer scale factor of the missile-borne RINS with fiber optic gyro. Optics Express, 2016, 24(19):21228-21243.doi:10.1364/OE.24.021228
申请国家发明7项,已授权4项(其中第1发明人1项)