航空宇航信息与控制系
王伟

王伟

职       务:长聘教轨副教授、博导

电子邮件:wangwei215661@sjtu.edu.cn

办公地址:上海交通大学太阳集团tyc151学院A242室

 

工作经历

时间 任职单位 职务
2021年-至今 上海交通大学太阳集团tyc151学院 长聘教轨副教授
2019年-2021年 清华大学航天航空学院 博士后助理研究员

教育背景

时间 毕业院校 学历
2014年-2018年 西北工业大学 博士
2015年-2017年 比萨大学 博士联合培养
2010年-2013年 西北工业大学 硕士
2006年-2010年 西北工业大学 本科

研究方向

(1)航天动力学与控制;

(2)航天器/无人机编队与集群飞行;

(3)深空探测轨道设计与优化;

(5)小行星动力学与控制;

(6)空间引力波探测轨道设计;

(7)太阳帆、电动帆航天器任务分析。

主要科研项目

(1)国家自然科学基金面上项目(No.12272223),主持

(2)国家自然科学基金青年项目(No.11902175),主持

(3)国家重点研发计划“引力波探测”重点专项青年科学家项目-任务课题(No.2022YFC2204800),主持

(4)博士后科学基金面上项目(No.2019M650700),主持

(5)博士后创新人才支持计划项目(No.BX20190166),主持

(6)上海市自然基金面上项目(No.23ZR1433600),主持

(7)太阳集团tyc151结构力学及控制全国重点实验室开放课题(No.MCMS-E-0223G01),主持

(8)国家杰出青年科学基金项目(No.11525208),参与。

代表性论文专著

(1)​Wang W, Wu D, Lei H and Baoyin H*. Fuel-Optimal Spacecraft Cluster Flight Around an Ellipsoidal Asteroid [J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (10): 1875–1882.

(2)Wang W, Mengali G, Quarta A A and Baoyin H*. Time-Optimal Formation Establishment Around a Slowly Rotating Asteroid [J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (4): 889–897.

(3)Wang W, Wu D, Mengali G, Quarta A A and Baoyin H*. Asteroid Hovering Missions from a Fuel-Consumption Viewpoint [J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (7): 1374–1382.

(4)Wang W, Yuan J*, Mengali G and Quarta A A. Invariant Manifold and Bounds of Relative Motion Between Heliocentric Displaced Orbits [J]. Journal of Guidance, Control, and Dynamics, 2016, 39 (8): 1764–1776.

(5)Gao C, Wang W, Yuan J* and Guo L. Hybrid Sail Displaced Orbits Around L2 Point in Elliptic Earth-Moon System [J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (2): 416–424.

(6)Sun R, Wang W* and Wang J. Distributed Control for Multiple Spacecraft System Near Asteroids with Event-Triggered Strategy [J]. Journal of Guidance, Control, and Dynamics, 2024, 47 (5): 1005–1014.

(7)Wang W, Lei H, Mengali G, Quarta A A and Baoyin H*. Along-Track Boundedness Condition for Spacecraft Relative Motion Around a Slowly Rotating Asteroid [J]. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59 (1): 497–506.

(8)Wang W, Wu D*, Sun R* and Baoyin H. Optimal Projected Circular Orbit for Spacecraft Formation Flying Near A Slowly Rotating Asteroid [J]. IEEE Transactions on Aerospace and Electronic Systems, 2022, 58 (6): 5483–5493.

(9)Wang W*, Mengali G, Quarta A A and Baoyin H. Spacecraft Relative Motion Control Near an Asteroid with Uncertainties: A Lyapunov Redesign Approach [J]. IEEE Transactions on Aerospace and Electronic Systems, 2024, In press.

(10)Wang W, Baoyin H*, Mengali G and Quarta A A. Solar Sail Cooperative Formation Flying Around L2-Type Artificial Equilibrium Points [J]. Acta Astronautica, 2020, 169: 224–239.

(11Wang W, Quarta A A, Mengali G* and Yuan J. Multiple Solar Sail Formation Flying Around Heliocentric Displaced Orbit via Consensus [J]. Acta Astronautica, 2019, 154: 256–267.

(12Wang W, Mengali G, Quarta A A and Yuan J*. Distributed Adaptive Synchronization for Multiple Spacecraft Formation Flying Around Lagrange Point Orbits [J]. Aerospace Science and Technology, 2018, 74: 93–103.

(13Wang W, Mengali G, Quarta A A and Baoyin H*. Decentralized Fault-Tolerant Control for Multiple Electric Sail Relative Motion at Artificial Lagrange Points [J]. Aerospace Science and Technology, 2020, 103: 105904.

(14Wang W, Mengali G, Quarta A A* and Yuan J. Analysis of Relative Motion in Non-Keplerian Orbits via Modified Equinoctial Elements [J]. Aerospace Science and Technology, 2016, 58: 389–400.

(15Wu D, Wang W*, Jiang F* and Li J. Minimum-Time Low-Thrust Many-Revolution Geocentric Trajectories with Analytical Costates Initialization [J]. Aerospace Science and Technology, 2021, 119: 107146.

(16Wang W, Mengali G*, Quarta A A and Yuan J. Formation Flying for Electric Sails in Displaced Orbits. Part I: Geometrical Analysis [J]. Advances in Space Research, 2017, 60 (6): 1115–1129.

(17Wang W, Mengali G*, Quarta A A and Yuan J. Formation Flying for Electric Sails in Displaced Orbits. Part II: Distributed Coordinated Control [J]. Advances in Space Research, 2017, 60 (6): 1130–1147.

(18Wang W, Mengali G, Quarta A A* and Yuan J, Extreme Values of Relative Distances for Spacecraft in Elliptic Displaced Orbits [J]. Advances in Space Research, 2016, 58 (4): 475–487.

(19Wu Y, Wang W*, Zhu H, Wu S*, and Damaren C J. Adaptive Fault-Tolerant Control for Spacecraft Formation under External Disturbances with Guaranteed Performance [J]. Advances in Space Research, 2023, 72 (5): 1583–1592.

(20Zhang J, Yuan J*, Wang W and Wang J. Reachable Domain of Spacecraft with aSingle Normal Impulse [J]. Aircraft Engineering and Aerospace Technology, 2019, 91 (7): 977–986.

(21)王伟,袁建平*,罗建军. 航天器集群编队最优单脉冲机动 [J]. 力学学报,2015,47 (5): 799–806.

(22)武迪,程林,王伟,李俊峰*. 基于切换系统的小推力轨迹优化协态初始化方法 [J]. 深空探测学报,2021,8 (5): 528–533.

 

学术兼职

(1)AIAA高级会员;中国力学学会会员;中国宇航学会会员;中国振动工程学会会员;

(2)《Astrodynamics》青年编委;《Aerospace》等3本SCI期刊专刊客座编委;

(3)国际自主无人系统大会分会场主席;

(4)国家自然科学基金委函评专家;

(5)全国研究生教育评估监测专家。

 

荣誉奖励

(1)博士后创新人才支持计划,2019年;

(2)陕西省科学技术一等奖,2016年;

(3)上海市青年五四奖章集体;

(4)中国国际大学生创新大赛银奖指导教师;

(5)中国国际大学生创新大赛上海赛区优秀指导教师;

(6)“挑战杯”中国大学生创业计划竞赛金奖指导教师。

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技术支持:维程互联