孙秀聪

职称\职位:讲师\硕士生导师
出生年月:1988年4月
电子邮箱:xiucong.sun@buaa.edu.cn
办公地点:北航沙河校区主楼D801
办公电话:


基本情况

教育经历
2017年获北京航空航天大学飞行器设计专业博士学位
工作经历
2017年7月至今，北京航空航天大学宇航学院，讲师，硕士生导师
研究方向

1、 飞行器自主导航
2、 航天器精密轨道确定
3、 轨道动力学与控制
4、 GPS与北斗导航定位技术
主讲课程

本科生课程《姿态与轨道动力学》
研究生课程《轨道确定原理与方法》
科研成果

主持国家自然科学基金、北京市自然科学基金等纵向项目4项，中科院、航天科技一院、航天科工四院等横向项目6项
获奖情况

2019-10，中国卫星导航定位协会卫星导航定位科技进步奖二等奖
代表论文

发表SCI/EI检索论文29篇：
SCI论文列表：
[1] 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
[2] 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
[3] 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
[4] 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
[5] 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
[6] 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
[7] 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
[8] 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
[9]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
[10] 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
[11] 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
[12]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
[13] 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
[14]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
[15]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
[16]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
[17]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
[18] 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
代表专利

申请发明专利6项，授权3项