教育背景
[1] 1999.9-2003.7
天津大学 | 电子科学与技术 | 学士学位 | 本科
[2] 2003.9-2005.12
国防科学技术大学 | 控制科学与工程 | 硕士学位 | 硕士研究生毕业
[3] 2006.2-2010.12
国防科学技术大学 | 光学工程 | 博士学位 | 博士研究生毕业
[4] 2008.3-2010.3
澳大利亚新南威尔士大学 | 导航制导与控制 | 博士联合培养
工作经历
[1] 2018.9-至今
航空航天学院 | 中南大学 副教授
[2] 2018.1-2018.9
航空航天学院 | 中南大学 讲师
[3] 2010.12-2017.12
光电科学与工程学院 | 国防科学技术大学 讲师
项目课题经历
主要研究方向为惯性导航及组合导航理论与技术,在激光陀螺/光纤陀螺惯导系统设计和应用领域具有多年的科研积累,系统研究了惯导的高精度标定与误差补偿技术、惯导扰动基座和动基座上的初始对准技术、惯导动态误差分析与误差分离技术、惯导误差的旋转调制补偿技术、基于惯导的多传感器融合导航技术,解决了惯导在航海导航、陆用定位定向、航空航天导航等应用领域的一系列关键理论和技术问题
论文、成果、著作等
[1] Songlai Han, Jinling Wang. Integrated GPS/INS Navigation System with Dual-Rate Kalman Filter [J]. GPS Solutions, 2012, 16(3): 389-404
[2] Songlai Han, Jinling Wang. A Novel Method to Integrate IMU and Magnetometers in Attitude and Heading Reference Systems [J]. The Journal of Navigation, 2011, 64(4): 727-738
[3] Songlai Han, Jinling Wang. Quantization and Colored Noises Error Modeling for Inertial Sensors for GPS/INS Integration [J]. IEEE Sensors Journal, 2011, 11(6):
[4] Songlai Han, Jinling Wang. A Novel Initial Alignment Scheme for Low-Cost INS Aided by GPS for Land Vehicle Applications [J]. The Journal of Navigation, 63(4):
[5] Songlai Han and Jinling Wang. Land Vehicle Navigation with the Integration of GPS and Reduced INS: Performance Improvement with Velocity Aiding [J]. The Journal of Navigation, 63(1): 153–166
[6] Songlai Han, Jinling Wang. A Novel Initial Alignment Method for GPS/INS Integration with Large Initial Heading Error [C]. 22nd International Meeting of ION, 2009, 935-945
[7] Songlai Han, Jinling Wang, Nathan Knight. Using Allan Variance to Determine the Calibration Model of Inertial Sensors for GPS/INS Integratoin [C]. 6th International Symposium on MMT, 2009,
[8] Songlai Han, Jinling Wang. Monitoring the Degree of Observability in Integrated GPS/INS Systems [C]. International Symposium on GPS/GNSS 2008, 2008, 414-421
[9] Zhichao Zheng, Songlai Han, Jin Yue, Lilong Yuan. Compensation for Stochastic Error of Gyros in a Dual-axis Rotational Inertial Navigation System [J]. The Journal of Navigation, 2016, 69(1): 169-182
[10] Zhichao Zheng, Songlai Han, Kefei Zheng. An Eight-Position Self-Calibration Method for a Dual-Axis Rotational Inertial Navigation System [J]. Sensors and Actuators: A-Physical, 2015, 39-48
[11] Guyi Rao, Guochen Wang, Songlai Han, Wen Zhang. Calibration of Laser Inertial Navigator with Dual-axis Rotation [J]. International Journal of CAS, 2015, 13(4): 960-966
[12] Wang Guochen, Rao Guyin, Han Songlai, Zhang Mei, Yuan Baolun. Research on the Thermal Relaxation Effect of Nonplanar Four-Frequency Differential Laser Gyro [J]. Applied Optics, 2013, 52(19): 4549-4555
[13] Baolun Yuan, Dan Liao, and Songlai Han. Error Compensation of Optical Gyro INS by Multi-Axis Rotation [J]. Measurement Science and Technology, 2012, 23(2): 1-9
[14] Baolun Yuan, Songlai Han, Jianqiang Yang, Danliao. Rotation Scheme for Single-Axis Indexing RLG INS [J]. Journal of Chinese Inertial Technology, 2011, 19(2): 145-151
[15] Nathan Knight, Jinling Wang, Chris Rizos and Songlai Han. GNSS Integrity Monitoring for Two Satellite Faults [C]. IGNSS Symposium 2009, 2009,
[16] Weidong Ding, Jinling Wang, Songlai Han, Ali Almagbile et.al. Adding Optical Flow into the GPS/INS Integration for UAV navigation [C]. IGNSS Symposium 2009, 2009,
[17] Jinling Wang,Matthew Garratt,Andrew Lambert,Jack Jianguo Wang,Songlai Han,David Sinclair. Integration of GPS/INS/Vision sensors to navigate Unmanned Aerial Vehicles [C]. XXI Congress of ISPRS, 2008, 963-970
专利、著作版权等
[1]自动补偿XX误差的三轴转位控制方法
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