教育经历
[1] 2007.9-2012.5北京航空航天大学 | 精密仪器及机械 | 博士学位 | 博士研究生毕业
[2] 2003.9-2007.7
北京航空航天大学 | 探测制导与控制技术 | Bachelor's Degree | 本科
工作经历
[1] 2012.8-2014.3中航工业西安飞行自动控制研究所（618所） |导航部 |高精度导航技术系统工程师
[2] 2014.3-2016.3
北京航空航天大学 |电子信息工程学院 |博士后
[3] 2016.3-至今
北京航空航天大学 |仪器科学与光电工程学院 |精密仪器及机械 教师
研究方向
[1] 组网协同技术[2] 多源组合导航技术
[3] 多源信息融合导航
[4] 卫星导航与测量
[5] 新型惯性导航与测量技术
团队成员
北京航空航天大学惯性导航与组合导航实验室北京航空航天大学仪器科学与光电工程学院冯培德院士团队
冯培德
王玮
张京娟
王蕾
王学运
陈刚
研究领域
当前位置: 中文主页 >> 研究领域新型惯性导航与测量技术、卫星导航与测量技术、多源信息融合技术、组网协同技术
开授课程
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科研项目
当前位置: 中文主页 >> 科研项目[1] 基于测距网络的飞机集群编队分布式协同导航方法研究, 2019/01/01-2021/12/31, 在研
[2] xxxxxxx惯性导航技术-2020/12/31, 在研
[3] 无依托快速xxx的技术研究-2019/12/31, 在研
[4] 新一代空中交通管理技术发展的战略研究-2016/03/31, 结题
[5] 基于GNSS/INS的机载多星座多源深组合导航关键技术研究-2017/12/31, 结题
[6] 光纤陀螺惯性导航系统样机试验-2018/03/31, 结题
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论文
当前位置: 中文主页 >> 论文[1] A Rapid and High-Precision Initial Alignment Scheme for Dual-axis Rotational Inertial Navigation System. Microsystem Technologies, 2017: 1-11.
[2] Four-position heading effect calibration algorithm for rotation inertial navigation system based on fiber optic gyro. Optical Engineering, 2016, 55(7): 074105-1-074105-10.
[3] Identifying Z-axis gyro drift and scale factor error using azimuth measurement in fiber optic gyroscope single-axis rotation inertial navigation system. Optical Engineering, 2017, 56(2): 024102-1-024102-10.
[4] Self-calibration method of inner lever-arm parameters for tri-axis RINS. Measurement Science and Technology, 2017, 2: 1-10.
[5] A self-calibration method for tri-axis rotational inertial navigation system. Measurement Science and Technology, 2016, 27:1-10.
[6] Single-axis rotation/azimuth-motion insulation inertial navigation control system with FOGs. Optics Express, 2017, 25(25): 30956-30975.
[7] Analysis and experiment of error restraint principle in an inertial navigation system with inertial sensors rotation. Int. J. Sensor Networks, 2016, 21(2): 127-136.
[8] Analysis and Improvement of Attitude Output Accuracy in Rotation Inertial Navigation System, Mathematical Problems in Engineering. 2015: 1-10.
[9] Research on Parameter Estimation Methods for Alpha Stable Noise in a Laser Gyroscope’s Random Error. Sensors, 2015, 15: 18550-18564.
[10] Research on the Rapid and Accurate Positioning and Orientation Approach for Land Missile-Launching Vehicle. Sensors, 2015, 15: 26606-26620.
[11] Rapid detection of index for encoder in rotary inertial navigation system. Optics Express, 2016, 24(5): 5591-5599.
[12] Study on Integration of FOG Single-axis Rotational INS and Odometer for Land Vehicle. IEEE Sensors Journal, 2018, 18(2): 752-763.
[13] Soft Fault Diagnosis and Recovery Method Based on Model Identification in Rotation FOG Inertial Navigation System. IEEE Sensors Journal, 2017, 17(17): 5705-5716.
[14] A Self-Calibration Method for Non-Orthogonal Angles of Gimbals in Tri-Axis Rotational Inertial Navigation System. IEEE Sensors Journal, 2016, 16(24): 8998-9005.
[15] An Accelerometers Size-Effect Self-Calibration Method for Tri-axis Rotational Inertial Navigation System. IEEE Transactions on Industrial Electronics, 2018, 65(2): 1655-1664.
[16] Online self-calibration research of single-axis rotational inertial navigation system. Measurement, 2018, 129: 633-641.
[17] The Asynchronous Gimbal-Rotation-Based Calibration Method for Lever-Arm Errors of Two Rotational Inertial Navigation System. IEEE Access, 2019, 7: 4653-4663.
[18] An inertial device biases on-line monitoring method in the applications of two rotational inertial navigation systems redundant configuration, Mechanical Systems And Signal Processing, 2019,120: 133-149.
[19] A Self-Calibration Method for Accelerometer Nonlinearity Errors in Tri-axis Rotational Inertial Navigation System. IEEE Transactions on Instrumentation and Measurement, 2017, 66(2): 243-253.
[20] A novel redundant INS based on triple rotary inertial measurement units. Measurement Science and Technology, 2016, 27: 1-12.
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荣誉及奖励
当前位置: 中文主页 >> 荣誉及奖励[1]中国仪器仪表学会金国藩青年学子奖
[2]北京航空航天大学优秀博士后
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