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。
[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.
