在读研期间，所有与你读研相关的事情，可能都需要经过你的导师同意，所以说，选择导师真的很重要，也希望大家能够认真对待这件事，怎样才能选择适合自己的导师呢?这就要我们提前做足功课，尽可能多的搜集有关你准备报考的导师的信息，下面新东方在线考研频道为大家分享：“北京理工大学硕士研究生导师信息：齐毅”文章。
齐毅
所在学科：航空宇航科学与技术
联系电话：
通讯地址：中关村南路5号北京理工大学宇航楼职 称：预聘副教授
邮 箱：qiyi08@bit.edu.cn
邮 编：100081教育经历
2012年9月-2017年6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
2008年9月-2012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
2020年11月-至今，北京理工大学宇航学院 预聘副教授
2017年9月-2020年9月，加拿大瑞尔森大学 博士后研究员
主要研究领域
1、深空探测航天器轨道动力学
2、日地月限制性四体问题下航天器轨道优化设计与控制
3、太阳系小天体运动
获奖情况
1、2018年，北京航空航天大学2018年校级优秀博士学位论文获得者。
社会兼职
SCI期刊审稿人：Monthly Notices of the Royal Astronomical Society, Journal of Guidance, Control, and Dynamics, Aerospace Science and Technology, Acta Astronautica, Celestial Mechanics and Dynamical Astronomy等。
近年来主要发表论文
[1]. Qi Y, de Ruiter A. Lunar flyby transfers to L5 axial orbit [J]. Acta Astronautica, 2021, 180: 516-526.
[2]. Qi Y, de Ruiter A. Optimal Powered Aerogravity-Assist Trajectories[J]. Journal of Guidance, Control, and Dynamics, 2020: 1-12
[3]. Zotos E E, Qi Y, Steklain A F, et al. Determining the nature of motion around Jupiter-like exoplanets using the elliptic restricted three-body problem[J]. Planetary and Space Science, 2020, 187: 104945.
[4]. Qi Y, de Ruiter A. A new understanding of L 4 and L 5 axial orbits through the torus structure[J]. Monthly Notices of the Royal Astronomical Society, 2020, 498(4): 5343-5352.
[5]. Qi Y, de Ruiter A. Phase structure of co-orbital motion with Jupiter[J]. Monthly Notices of the Royal Astronomical Society, 2020, 494(4): 4695-4705.
[6]. Qi Y, de Ruiter A. Achievable Halo Phasing with Short-Range Trajectories[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(5): 928-938.
[7]. Qi Y, de Ruiter A. Kozai mechanism inside mean motion resonances in the three-dimensional phase space[J]. Monthly Notices of the Royal Astronomical Society, 2020, 493(4): 5816-5824.
[8]. Qi Y, de Ruiter A. Powered Swing-By with Continuous Thrust[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(1): 111-121.
[9]. Qi Y, de Ruiter A. Station-keeping strategy for real translunar libration point orbits using continuous thrust[J]. Aerospace Science and Technology, 2019, 94: 105376.
[10]. Qi Y, de Ruiter A. Planar near-Earth asteroids in resonance with the Earth[J]. Icarus, 2019, 333: 52-60.
[11]. Qi Y, de Ruiter A. Transfers to Lunar Libration Point Orbits [J]. Communications in Nonlinear Science and Numerical Simulation, 2019, 74: 180-200.
[12]. Zotos E E, Qi Y*. Near-optimal capture in the planar circular restricted Pluto-Charon system[J]. Planetary and Space Science, 2019, 165: 85-98.
[13]. Qi Y, de Ruiter A. Short-term capture of the Earth–Moon system[J]. Monthly Notices of the Royal Astronomical Society, 2018, 476(4): 5464-5478.
[14]. Qi Y, de Ruiter A. Energy analysis in the elliptic restricted three-body problem[J]. Monthly Notices of the Royal Astronomical Society, 2018, 478(1): 1392-1402.
[15]. Qi Y, Ruiter A. Study of Correction Maneuver for Lunar Flyby Transfers in the Real Ephemeris[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(10): 2112-2132.
[16]. Qi Y, de Ruiter A. Powered swing-by in the elliptic restricted three-body problem[J]. Monthly Notices of the Royal Astronomical Society, 2018, 481(4): 4621-4636.
[17]. Qi Y, de Ruiter A. Low-energy transfers to long-term capture in the Earth-Moon system[J]. Acta Astronautica, 2018, 152: 836-849.
[18]. Qi Y, Xu S, Qi R. Lunar flyby transfers between libration point orbits[J]. Monthly Notices of the Royal Astronomical Society, 2017, 468(2): 2265-2282.
[19]. Qi Y, Xu S. Optimal earth-moon transfers using lunar gravity assist in the restricted four-body problem[J]. Acta Astronautica, 2017, 134: 106-120.
[20]. Qi Y, Xu S, Qi R. Transfer from Earth to libration point orbit using lunar gravity assist[J]. Acta Astronautica, 2017, 133: 145-157.
[21]. Qi Y, Xu S. Earth–Moon transfer with near-optimal lunar capture in the restricted four-body problem[J]. Aerospace Science and Technology, 2016, 55: 282-291.
[22]. Qi Y, Xu S. Study of lunar gravity assist orbits in the restricted four-body problem[J]. Celestial Mechanics and Dynamical Astronomy, 2016, 125(3): 333-361.
[23]. Qi Y, Xu S. Minimum ΔV for the transfer to permanent lunar orbits with hyperbolic approach[J]. Acta Astronautica, 2016, 119: 183-195.
[24]. Qi Y, Xu S. Mechanical analysis of lunar gravity assist in the Earth–Moon system[J]. Astrophysics and Space Science, 2015, 360(2): 55.
[25]. Qi Y, Xu S. Long-term behavior of the spatial orbit near the Moon in restricted three-body problem[J]. Astrophysics and Space Science, 2015, 359(1): 19.
[26]. Qi Y, Xu S. Lunar capture in the planar restricted three-body problem[J]. Celestial Mechanics and Dynamical Astronomy, 2014, 120(4): 401-422.
[27]. Qi Y, Xu S J, Qi R. Gravitational lunar capture based on bicircular model in restricted four body problem[J]. Celestial Mechanics and Dynamical Astronomy, 2014, 120(1): 1-17.
[28]. 齐毅, 徐世杰. 准双椭圆三体模型[J]. 中国科学:物理学,力学,天文学, 2020(7):98-107.
以上就是小编为大家分享的：“北京理工大学硕士研究生导师信息：齐毅”，更多研究生导师信息，欢迎继续浏览新东方在线研究生导师频道。