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个人简介

工作经历 时间 任职单位 职务 2021年-至今 上海交通大学航空航天学院 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 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)国家杰出青年科学基金项目(No.11525208),参与; (7)欧盟第七框架项目(No.262733),参与。 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)全国航天飞行动力学技术研讨会优秀论文,2014年。

研究领域

(1)航天动力学与控制; (2)卫星编队/集群飞行; (3)深空探测轨道设计与优化; (4)小行星动力学与控制; (5)空间引力波探测轨道设计; (6)太阳帆、电动帆航天器任务分析。

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)

(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)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. (7)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. (8)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. (9)Wang 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. (10)Wang 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. (11)Wang 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. (12)Wang 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. (13)Wu 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. (14)Wang 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. (15)Wang 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. (16)Wang 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. (17)Zhang J, Yuan J*, Wang W and Wang J. Reachable Domain of Spacecraft with a Single Normal Impulse [J]. Aircraft Engineering and Aerospace Technology, 2019, 91 (7): 977–986. (18)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. (19)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)国内外航空航天领域期刊和会议审稿人和编辑顾问; (2)“意大利高校研究-工业和信息工程领域”评阅人。

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