Cao Songyin
Gender:Male
Alma Mater:Southeast University
Paper Publications
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Cao Songyin,季辰一,高红莲.基于GPS/偏振/地磁信息的SINS AUKF-ASVSF 空中对准方法.中国惯性技术学报,2023,31(12)1181-1188.
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Cao Songyin,高红莲,裔扬.Adaptive In-Flight Alignment Method for SINS/GPS/Polarization Integrated Navigation System Based on the Degree of Observability Analysis.IEEE SENSORS JOURNAL,2023,23(15)16699-16709.
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Cao Songyin,高红莲.Adaptive In-Flight Alignment Method for SINS/GPS/Polarization Integrated Navigation System Based on the Degree of Observability Analysis.IEEE SENSORS JOURNAL,2023,23(15)16699-16709.
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Cao Songyin,高红莲,尤杰.In-Flight Alignment of Integrated SINS/GPS/Polarization/Geomagnetic Navigation System Based on Federal UKF.SENSORS,2022,22(16)
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Cao Songyin,郭雷,丁正桃.Event-triggered anti-disturbance attitude control for rigid spacecrafts with multiple disturbances.INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL,2021,31(2)344-357.
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FY,Cao Songyin,Pat Wheele.Sliding Mode Controller Applied to Coupled Inductor Dual Boost Inverters.JOURNAL OF POWER ELECTRONICS,2019,19(6)1403-1412.
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Cao Songyin,杭斌.Adaptive fault tolerant attitude control of flexible satellites based on Takagi-Sugeno fuzzy disturbance modeling.TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL,2020,42(9)1712-1723.
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Cao Songyin,刘俊,裔扬.Non-singular terminal sliding mode adaptive control of permanent magnet synchronous motor based on a disturbance observer.The Journal of Engineering,2019,2019(15)629-634.
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Cao Songyin,郭雷,陈文华.Anti-disturbance fault tolerant initial alignment for inertial navigation system subjected to multiple disturbances.AEROSPACE SCIENCE AND TECHNOLOGY,2018,7295-103.
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Cao Songyin,赵云枫.Anti-disturbance fault-tolerant attitude control for satellites subject to multiple disturbances and actuator saturation.NONLINEAR DYNAMICS,2017,89(4)2657-2667.
