孙秀聪 - 北京航空航天大学

个人简介

孙秀聪，北京航空航天大学航天飞行器技术系副研究员、硕士生导师。2010年7月和2017年3月分别获北京航空航天大学飞行器设计专业学士和博士学位（导师为韩潮教授）。2019年入选北京航空航天大学“青年拔尖人才支持计划”。主讲本科生课程“姿态与轨道动力学”和研究生课程“非线性滤波理论及航天应用”。长期从事航天器/飞行器自主导航以及最优滤波理论的研究工作。主持国家自然科学基金、国防科技重点实验室基金、北京市自然科学基金等纵向项目以及航天一院、中科院空间科学中心等单位横向项目十余项；作为有效载荷分系统负责人参与亚太空间合作组织APSCO大学生小卫星项目（卫星于2021年10月14日成功发射）。发表SCI论文30余篇，授权发明专利5项。曾获中国卫星导航定位科技进步奖二等奖（2019）、空军“创新杯”科技创新大赛一等奖（2021）。教育经历 2006.9 -- 2010.7 北京航空航天大学飞行器设计专业本科毕业学士学位 2010.9 -- 2017.3 北京航空航天大学飞行器设计专业博士研究生毕业博士学位工作经历 2017.7 -- 2021.7 北京航空航天大学宇航学院讲师 2021.8 -- 至今北京航空航天大学宇航学院副研究员

研究领域

航天器轨道/姿态确定飞行器组合导航非合作目标跟踪最优滤波理论导航信息处理与系统开发

近期论文

查看导师新发文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Bai, S., Han, C., Rao, Y.,Sun, X., and Sun, Y., “New Fly-Around Formations for an Elliptical Reference Orbit,”Acta Astronautica, Vol. 171, Jun. 2020, pp. 335-351. (SCI, Q1, IF2018: 2.482) doi:10.1016/j.actaastro.2020.03.008 Han, C., Wang, Y., Chen, H.,Sun, X., Sun, Y., and Li, J., “Practical Low-Thrust Geostationary Orbit Transfer Guidance via Linearized State Equations,”Journal of Guidance, Control, and Dynamics, Vol. 43, No. 3, Mar. 2020, pp. 620-627. (SCI, Q2, IF2018: 2.061) doi:10.2514/1.G004692 Han, C., Bai, S.,Sun, X.(corresponding author), and Rao, Y., “Hovering Formation Control Based on Two-Stage Constant Thrust,”Journal of Guidance, Control, and Dynamics, Vol. 43, No. 3, Mar. 2020, pp. 504-517. (SCI, Q2, IF2018: 2.061) doi:10.2514/1.G004595 Zhang, R., Han, C., andSun, X.(corresponding author), “Initial Orbit Determination from Atmospheric Drag Direction,”Journal of Guidance, Control, and Dynamics, Vol. 42, No. 12, Dec. 2019, pp. 2731-2740. (SCI, Q2, IF2018: 2.061) doi:10.2514/1.G004530 Wang, X., Han, C., Yang, P., andSun, X., “Onboard Satellite Visibility Prediction Using Metamodeling Based Framework,”Aerospace Science and Technology, Vol. 94, Nov. 2019, 105377. (SCI, Q1, IF2018: 2.829) doi:10.1016/j.ast.2019.105377 Wang, H., Han, C., andSun, X.(corresponding author), “Analytical Field-of-Regard Representation for Rapid and Accurate Prediction of Agile Satellite Imaging Opportunities,”Journal of Astronomical Telescopes, Instruments, and Systems, Vol. 5, No. 3, Jul.-Sep. 2019, 037001. (SCI, Q1, IF2018: 3.143) doi:10.1117/1.JATIS.5.3.037001 Chen, H., Han, C., Rao, Y., Yin, J., andSun, X.(corresponding author), “Algorithm of Relative Lambert Transfer Based on Relative Orbital Elements,”Journal of Guidance, Control, and Dynamics, Vol. 42, No. 6, Jun. 2019, pp. 1413-1422. (SCI, Q2, IF2018: 2.061) doi:10.2514/1.G003348 Zhang, S., Han, C., andSun, X.(corresponding author), “New Solution for Rendezvous Between Geosynchronous Satellites Using Low Thrust,”Journal of Guidance, Control, and Dynamics, Vol. 41, No. 6, Jun. 2018, pp. 1396-1405. (SCI, Q2, IF2018: 2.061) doi:10.2514/1.G003270 Sun, X., Han, C., and Chen, P., “Real-Time Precise Orbit Determination of LEO Satellites Using a Single-Frequency GPS Receiver: Preliminary Results of Chinese SJ-9A Satellite,”Advances in Space Research, Vol. 60, No. 7, Oct. 2017, pp. 1478-1487. (SCI, Q3, IF2018: 1.746) doi:10.1016/j.asr.2017.06.052 Chen, P., Sun, T., andSun, X.(corresponding author), “Autonomous Orbit Determination Using Epoch-Differenced Gravity Gradients and Starlight Refraction,”Chinese Journal of Aeronautics, Vol. 30, No. 5, Oct. 2017, pp. 1740-1749. (SCI, Q1, IF2018: 2.095) doi:10.1016/j.cja.2017.07.003 Zhou, K.,Sun, X., Huang, H., Wang, X., and Ren, G., “Satellite Single-Axis Attitude Determination Based on Automatic Dependent Surveillance-Broadcast Signals,”Acta Astronautica, Vol. 139, Oct. 2017, pp. 130-140. (SCI, Q1, IF2018: 2.482) doi:10.1016/j.actaastro.2017.05.038 Sun, X., Han, C., and Chen, P., “Precise Real-Time Navigation of LEO Satellites Using a Single-Frequency GPS Receiver and Ultra-Rapid Ephemerides,”Aerospace Science and Technology, Vol. 67, Aug. 2017, pp. 228-236. (SCI, Q1, IF2018: 2.829) doi:10.1016/j.ast.2017.04.006 Chen, P., Zhang, J., andSun, X.(corresponding author), “Real-Time Kinematic Positioning of LEO Satellites Using a Single-Frequency GPS Receiver,”GPS Solutions, Vol.21, No. 3, Jul. 2017, pp. 973-984. (SCI, Q2, IF2018: 3.049) doi:10.1007/s10291-016-0586-1 Sun, X., Han, C., and Chen, P., “Instantaneous GNSS Attitude Determination: A Monte Carlo Sampling Approach,”Acta Astronautica, Vol. 133, Apr. 2017, pp. 24-29. (SCI, Q1, IF2018: 2.482) doi:10.1016/j.actaastro.2017.01.006 Han, C., Gao, X., andSun, X.(corresponding author), “Rapid Satellite-to-Site Visibility Determination Based on Self-Adaptive Interpolation Technique,”Science China Technological Sciences,Vol. 60, No. 2, Feb. 2017, pp. 264-270. (SCI, Q2, IF2018: 2.180) doi:10.1007/s11431-016-0513-8 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, pp. 2436-2451. (SCI, Q1, IF2018: 2.797) doi:10.1109/TAES.2016.150387 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, IF2018: 2.482) doi:10.1016/j.actaastro.2016.03.012 Chen, P.,Sun, X.(corresponding author), 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, Q2, IF2018: 2.061) doi:10.2514/1.G001195