温昶煊 - 北京理工大学

个人简介

教育经历 2009年9月-2016年1月，在北京航空航天大学大学获得飞行器设计专业博士学位 2013年9月-2015年9月，在以色列理工学院航空航天工程系公派联合培养 2005年9月-2009年6月，在北京航空航天大学大学获得飞行器设计专业学士学位工作经历 2019年6月-至今，北京理工大学宇航学院 2016年3月-2019年5月，中国科学院空间应用工程与技术中心获奖情况 2017年，北京航空航天大学2017年校级优秀博士学位论文获得者

研究领域

航天器轨道可达范围的理论及其应用研究、卫星解体的碎片云演化模拟航天器在轨服务技术、小推力轨道转移技术、自主交会对接、近距离操作的碰撞风险评估编队和集群飞行动力学与控制

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）

WANG X, SHI P, WEN C. Design of Parameter-self-tuning Controller Based on Reinforcement Learning for Tracking Non-cooperative Targets in Space[J]. IEEE Transactions on Aerospace and Electronic Systems, 2020: 1. CHEN Q, QIAO D, WEN C. Orbital Element Reachable Set After Gravity Assists of Planets in Elliptical Orbits[J]. Journal of Guidance, Control, and Dynamics, 2020: 1–9. WEN C, MA J. Reachable domain for satellite relative motion along elliptic orbit with uncertainty and process noise[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020: 0954410019900726. WANG X, SHI P, WEN C. An Algorithm of Reinforcement Learning for Maneuvering Parameter Self-Tuning Applying in Satellite Cluster[J]. Mathematical Problems in Engineering, 2020, 2020: 1836159. CHEN Q, QIAO D, WEN C. Reachable Domain of Spacecraft After a Gravity-Assist Flyby[J]. Journal of Guidance, Control, and Dynamics, 2019, 42(4): 931–940. WEN. C, GAO. Y, SHI. H. Three-dimensional relative reachable domain with initial state uncertainty in Gaussian distribution[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(5): 1555–1570. WANG X, SHI P, WEN C. Adaptive control of coupled position and attitude for tracking characteristic point of disabled satellite[J]. ZhongguoKongjianKexueJishu/Chinese Space Science and Technology, 2018, 38(1). 王逍, 温昶煊, 赵育善等. 翻滚目标安全走廊内的碰撞可能性判断方法[J]. 哈尔滨工业大学学报, 2018(4). WEN C, PENG C, GAO Y. Reachable domain for spacecraft with ellipsoidal Delta-V distribution[J]. Astrodynamics, 2018, 2(3): 265–288. LEI B, SHI P, WEN C. Gain-Scheduling Attitude Control for Complex Spacecraft Based on HOSVD[J]. Journal of Dynamic Systems, Measurement, and Control, 2018. WEN C, GURFIL P. Guidance, navigation and control for autonomous R-bar proximity operations for geostationary satellites[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, 231(3): 452–473. WEN C, GURFIL P. Relative Reachable Domain for Spacecraft with Initial State Uncertainties[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(3): 462–473. WEN C, GURFIL P. Modeling Early Medium-Term Evolution of Debris Clouds Using the Reachable Domain Method[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(12): 2649–2660. WEN C, ZHANG H, GURFIL P. Orbit Injection Considerations for Cluster Flight of Nanosatellites[J]. Journal of Spacecraft and Rockets, 2015, 52(1): 196–208. WEN C, ZHAO Y, SHI P. Derivative Analysis and Algorithm Modification of Transverse-Eccentricity-Based Lambert Problem[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1195–1201. WEN C, ZHAO Y, SHI P. Orbital Accessibility Problem for Spacecraft with a Single Impulse[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1260–1271. WEN C, ZHAO Y, SHI P. Precise Determination of Reachable Domain for Spacecraft with Single Impulse[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(6): 1767–1779. WEN C, ZHAO Y, LI B. Solving the Relative Lambert’s Problem and Accounting for Its Singularities[J]. Acta Astronautica, 2014, 97(0): 122–129.