雷漢倫

雷漢倫

雷漢倫,男,1986年11月生,貴州遵義人,博士,現為南京大學天文與空間科學學院副教授,主持並參與多項自然基金項目。

基本介紹

  • 中文名:雷漢倫
  • 國籍中國
  • 出生地:貴州遵義
  • 出生日期:1986年11月
  • 畢業院校:南京大學
  • 學位/學歷:博士
  • 專業方向:天體力學
  • 任職院校:南京大學
  • 職稱:副教授
人物經歷,研究領域,承擔課程,學術成果,

人物經歷

2010年6月南京大學天文系本科畢業,2015年6月獲得南京大學天體力學博士學位,此後留系任教。2018年6月晉升為副教授。2017年12月至2018年12月期間在義大利羅馬大學航天工程系做訪問學者。曾獲2016年南京大學優秀博士論文。

研究領域

主要從事天體力學、航天動力學等領域的研究工作,包括複雜引力場環境下太空飛行器的軌道、姿態動力學,以及太陽系動力學等

承擔課程

《經典控制理論》

學術成果

最近三年(2016-2018)第一作者文章:
[1] Lei HL, Circi C, Ortore E., et al. quasi-frozen orbits around a slowly rotating asteroid, Journal of Guidance, Control and Dynamics, 2018.
[2] Lei HL, Circi C, Ortore E. Modified double-averaged Hamiltonian in hierarchical triple systems. Monthly Notices of the Royal Astronomical Society, 2018.
[3] Lei HL, Circi C, Ortore E, et al. Attitude stability and periodic attitudes of rigid spacecrafts on the stationary orbits around asteroid 216 Kleopatra. Advances in Space Research, 2018.
[4] Lei HL, Circi C, Ortore E, et al. Periodic attitudes and bifurcations of a rigid spacecraft in the second degree and order gravity field of a uniformly rotating asteroid. Celestial Mechanics and Dynamical Astronomy, 2018.
[5] Lei HL, Xu B, Circi C. Polynomial expansions of single-mode motions around equilibrium points in the circular restricted three-body problem. Celestial Mechanics and Dynamical Astronomy, 2018.
[6] Lei HL, Xu B. Resonance transition periodic orbits in the circular restricted three-body problem. Astrophysics and Space Science, 2018.
[7] Lei HL, Xu B. Low-energy transfers to cislunar periodic orbits visiting triangular libration points. Communications in Nonlinear Science and Numerical Simulation, 2018.
[8] Lei HL, Xu B, Zhang L. Trajectory design for a rendezvous mission to Earth’s Trojan asteroid 2010 TK7. Advances in Space Research, 2017.
[9] Lei HL, Xu B. Invariant manifolds around artificial equilibrium points for low-thrust propulsion spacecraft. Astrophysics and Space Science, 2017.
[10] Lei HL, Xu B. Families of impulsive transfers between libration points in the restricted three-body problem. Monthly Notices of the Royal Astronomical Society, 2016.
[11] Lei HL, Xu B. Transfers between libration point orbits of Sun–Earth and Earth–Moon systems by using invariant manifolds. Journal of Engineering Mathematics, 2016.

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