李魁 - 北京航空航天大学 - 仪器科学与光电工程学院

个人简介

主要从事惯性测量与导航技术研究、组合导航技术研究、多源信息融合技术研究等。作为主要完成人主持或承担了包括XXX国防973项目、XXX工程、国家自然科学基金、装备发展部预研基金、航天科工基金、XXX演示验证项目等多项国家级课题和重点型号研制。以第一作者/通信作者身份在国内外导航技术领域专业期刊上发表SCI索引论文30余篇，申请国家发明专利10余项。教育经历 2007.9 -- 2012.5 北京航空航天大学精密仪器及机械博士研究生毕业博士学位 2003.9 -- 2007.7 北京航空航天大学探测制导与控制技术本科学士学位工作经历 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 2014.3 -- 2016.3 北京航空航天大学电子信息工程学院博士后 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荣誉获奖中国仪器仪表学会金国藩青年学子奖北京航空航天大学优秀博士后科研项目基于测距网络的飞机集群编队分布式协同导航方法研究 xxxxxxx惯性导航技术无依托快速xxx的技术研究新一代空中交通管理技术发展的战略研究基于GNSS/INS的机载多星座多源深组合导航关键技术研究光纤陀螺惯性导航系统样机试验

研究领域

组网协同技术多源组合导航技术多源信息融合导航新型惯性导航与测量技术卫星导航与测量

近期论文

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A Rapid and High-Precision Initial Alignment Scheme for Dual-axis Rotational Inertial Navigation System. Microsystem Technologies, 2017: 1-11. 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. 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. Self-calibration method of inner lever-arm parameters for tri-axis RINS. Measurement Science and Technology, 2017, 2: 1-10. A self-calibration method for tri-axis rotational inertial navigation system. Measurement Science and Technology, 2016, 27:1-10. Single-axis rotation/azimuth-motion insulation inertial navigation control system with FOGs. Optics Express, 2017, 25(25): 30956-30975. 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. Analysis and Improvement of Attitude Output Accuracy in Rotation Inertial Navigation System, Mathematical Problems in Engineering. 2015: 1-10. Research on Parameter Estimation Methods for Alpha Stable Noise in a Laser Gyroscope’s Random Error. Sensors, 2015, 15: 18550-18564. Research on the Rapid and Accurate Positioning and Orientation Approach for Land Missile-Launching Vehicle. Sensors, 2015, 15: 26606-26620. Rapid detection of index for encoder in rotary inertial navigation system. Optics Express, 2016, 24(5): 5591-5599. Study on Integration of FOG Single-axis Rotational INS and Odometer for Land Vehicle. IEEE Sensors Journal, 2018, 18(2): 752-763. Soft Fault Diagnosis and Recovery Method Based on Model Identification in Rotation FOG Inertial Navigation System. IEEE Sensors Journal, 2017, 17(17): 5705-5716. 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. An Accelerometers Size-Effect Self-Calibration Method for Tri-axis Rotational Inertial Navigation System. IEEE Transactions on Industrial Electronics, 2018, 65(2): 1655-1664. Online self-calibration research of single-axis rotational inertial navigation system. Measurement, 2018, 129: 633-641. The Asynchronous Gimbal-Rotation-Based Calibration Method for Lever-Arm Errors of Two Rotational Inertial Navigation System. IEEE Access, 2019, 7: 4653-4663. 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. 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. A novel redundant INS based on triple rotary inertial measurement units. Measurement Science and Technology, 2016, 27: 1-12. Reinforced Ultra-Tightly Coupled GPS/INS System for Challenging Environment, Mathematical Problems in Engineering, 2014: 1-12. Federated ultra-tightly coupled GPS/INS integrated navigation system based on vector tracking for severe jamming environment. IET Radar, Sonar & Navigation, 2016: 1–8. FLIR/INS/RA Integrated Landing Guidance for Landing on Aircraft Carrier, International Journal of Advanced Robotic Systems, 2015, 12: 1-9. Enhanced Instrument Landing System Based on the Aided Inertial Navigation. Journal of Computational Information Systems, 2015,11(21):7873-7882. INS/ILS组合高精度进近着陆系统仿真研究. 计算机仿真. 2016, 33(4):95-100.