陈培 - 北京航空航天大学

个人简介

教育经历 2002/09-2007/07，北京航空航天大学，宇航学院，飞行器设计专业，博士 1998/09-2002/07，北京航空航天大学，宇航学院，学士工作经历 2016年12月Curtin University of Technology 在荷兰皇家科学院院士Peter Teunissen团队访问学者 2013/10至今，北京航空航天大学，宇航学院，航天飞行器技术系副主任 2011/10至今，北京航空航天大学，宇航学院，副教授 2007/08-2011/9，北京航空航天大学，宇航学院，讲师获奖情况 “JK863-2007721003”，省部级科技进步奖，获奖等级：一等， 2007年科研成果 GNSS导航技术。主持了包括国家自然基金、863子课题、973子课题和航天科技横向课题在内的二十多项与卫星导航系统相关的科研项目，已在《IEEE Transactions on Aerospace and Electronic Systems》、《GPS Solution》、《Aerospace Science and Technology》、《Journal of Guidance, Control, and Dynamics》、《IEEE Aerospace and Electronic System Magazine》、《Acta Astronautica》、《航空学报》、《宇航学报》、《北京航空航天大学学报》、《中国空间科学技术》发表科研论文二十多篇，第一发明人身份授权发明专利12项。具有丰富的航天工程经验, 曾参与国内/国际多个卫星型号的研制工作，在机械、电子技术方面也有长期积累,相关设计曾在国际比赛中获奖

研究领域

重力场自主导航技术、微小卫星技术、精密惯性载荷、GNSS导航技术

近期论文

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Chen, P., Sun, X., and Han, C, “Gravity Gradient Tensor Eigendecomposition for Spacecraft Positioning,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 11, Nov. 2015, pp. 2200-2206. (SCI, Q1) Chen, P., Sun, T., and Sun, X., “Autonomous Orbit Determination Using Epoch-Differenced Gravity Gradients and Starlight Refraction,”, Chinese Journal of Aeronautics in Jul. 2017. (SCI, Q2) Chen Pei, Shu Leizheng, Ding Ran and Han Chao, "Kinematic Single-frequency Relative Positioning for LEO Formation Flying Mission," GPS Solutions,2014, 19(4):525-535(SCI, Q1) Chen, P., Zhang, J., and Sun, X., “Real-Time Kinematic Positioning of LEO Satellites Using a Single-Frequency GPS Receiver,” GPS Solutions, 2017, 21(3): 973-984. (SCI, Q1) Sun, X., Chen, P., Macabiau, C., and Han, C., “Autonomous Orbit Determination via Kalman Filtering of Gravity Gradients,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 52, No. 5, Oct. 2016. (SCI, Q1) Chen Pei, “Attitude determination algorithms for spinning satellites using single antenna GPS receiver and MEMS gyro” Aerospace Science and Technology, 2013, 26(1):10-15. (SCI, Q1) Sun, X., Chen, P., Macabiau, C., and Han, C., “Low-Earth Orbit Determination from Gravity Gradient Measurements,” Acta Astronautica, Vol. 123, Jun.-Jul. 2016, pp. 350-362. (SCI, Q1) Sun, X., Han, C., and Chen, P., “Instantaneous GNSS Attitude Determination: A Monte Carlo Sampling Approach,” Acta Astronautica，2017，Vol. 133:24-29. (SCI, Q2) Sun, X., Han, C., Chen, P., “Precise Real-Time Navigation of LEO Satellites Using a Single-Frequency GPS Receiver and Ultra-Rapid Ephemerides”, Aerospace Science and Technology, 2017, 67(1):228-236. (SCI, Q1) Chen Pei., Wang, S., Han, C., “GNSS Baseband Logging System”, IEEE Aerospace and Electronics Systems Magazine, 2011,26(1):9–13. (SCI, Q2) Sun, X., Chen, P., Macabiau, C., and Han, C., “A Two-Tiered Approach to Spacecraft Positioning from Significantly Biased Gravity Gradient Measurements,” AAS/AIAA Astrodynamics Specialist Conference, Vail, CO, Aug. 2015, AAS 15-593. Sun, X., Chen, P., Sun, J., and Han, C., “GEO Orbit Determination Using BeiDou System,” 64th International Astronautical Congress, Beijing, China, Sep. 2013, IAC-13-B2.1.11. Shu, L., Chen, P., Sun, X., and Han, C., “Stochastic Modeling and Variance Component Estimation to GPS Observables for LEO Relative Navigation Applications,” AIAA Modeling and Simulation Technologies (MST) Conference, Boston, MA, Aug. 2013, AIAA 2013-5158. 陈培，王兴，空间2-RSSS机构的误差研究，北京航空航天大学学报，2011， 37(3) : 263-267 Shu LeiZheng, Chen Pei, Zhang Hongli and Han Chao, "Relative orbit determination for formation flying spacecraft using differenced BeiDou carrier phase,"Proceedings of 24th Spaceflight Mechanics Meeting, AAS/AIAA, Santa Fe, NM, Jan. 26-30, 2014. Shu LeiZheng, Chen Pei, Sun Xiu Cong, and Han Chao, "Stochastic modeling and variance component estimation to GPS observables for LEO relative navigation applications,"Proceedings of AIAA Modeling and Simulation Technologies (MST) Conference, Boston, MA, United States, Aug. 19-22, 2013. Shu LeiZheng, Chen Pei, Sun Xiu Cong, and Han Chao, "Stochastic Assessment of GPS Observations for LEO Relative Navigation,"Proceedings of 64th International Astronautical Congress, IAC, Beijing, China, Sep. 23-27, 2013