主讲课程
1、本科生课《航天器轨道动力学》，32学时
2、本科生课《航天器编队飞行理论》，32学时
3、研究生全英文课《Orbital Mechanics》，48学时
4、《航天器轨道动力学》中文慕课，学堂在线平台：
https://www.xuetangx.com/course/bit08201009942/
5、《Spacecraft Orbital Dynamics》英文慕课，学堂在线平台：
https://www.xuetangx.com/course/bit0820bt1119intl/
近年来主要发表论文
[1].Rui Qi*, Yang Zhang, Krishna D. Kumar. Design and Robustness Analysis of a Wave-Based Controller for Tethered Towing of Defunct Satellites, IEEE/CAA Journal of Automatica Sinica, 10(1): 278-280, 2023.
[2].张扬, 祁瑞*, 姚傅祯. 绳网拖曳带帆板失效卫星的波动控制, 宇航学报, 2022
[3].Rui Qi*, Fuzhen Yao, Shan Lu, Zehua Jiang. Stabilization of tethered tug-debris system with residual liquid fuel, Journal of Guidance, Control and Dynamics, 44(4): 880-888, 2021.
[4].Rui Qi*, Yang Zhang, Shan Lu, Quan Hu, Rui Zhong. Tethered towing of defunct satellites with solar panels, Acta Astronautica, 175: 1-10, 2020.
[5].Rui Qi*, Anrui Shi, Arun K. Misra, Krishna D. Kumar, Jingrui Zhang. Coulomb tether double-pyramid formation, a potential configuration for geostationary satellite collocation, Aerospace Science and Technology, 84: 1131-1140, 2019.
[6].Rui Qi*, Arun K. Misra, Zongyu Zuo. Active debris removal using double-tethered space-tug system, Journal of Guidance, Control and Dynamics, 40(3): 720-728, 2017.
[7].Rui Qi*, Arun K. Misra. Dynamics of double-pyramid satellite formation interconnected by tethers and coulomb forces, Journal of Guidance, Control and Dynamics, 39(6): 1265-1277, 2016.
[8].Rui Qi*, Biao Huang. Numerical investigation of transport mechanism in four-body problem using lagrangian coherent structure, Astrophysics and Space Science, 361(1): 1-9, 2016.
[9].Rui Qi*, Shijie Xu. Optimal low-thrust transfers to lunar L1 halo orbit using variable specific impulse engine, Journal of Aerospace Engineering, 28(4): 04014096, 2015.
[10].Rui Qi*, Shijie Xu. Applications of lagrangian coherent structures to expression of invariant manifolds in astrodynamics, Astrophysics and Space Science, 351: 125-133, 2014.
[11].Rui Qi*, Shijie Xu, Tong Chen. Control of orientation for spacecraft formations in the vicinity of the Sun-Earth L2 libration point, Science China: Physics, Mechanics & Astronomy, 57(9): 1778-1787, 2014.
[12].Rui Qi*, Shijie Xu, Ming Xu. Impulsive control for formation flight about libration points, Journal of Guidance, Control and Dynamics, 35(2): 484-496, 2012.
[13].Jingrui Zhang, Keying Yang, Rui Qi*. Dynamics and Offset Control of Tethered Space-Tug System, Acta Astronautica, 142: 232-252, 2018.
[14].Hao Zeng, Jingrui Zhang, Rui Qi*, Mingtao Li. Study of time-free transfers into libration point orbits with multiple constraints, Journal of Guidance, Control and Dynamics, 40(11): 2752-2770, 2017.
[15].Yi Qi*, Shijie Xu*, Rui Qi*. Lunar flyby transfers between libration point orbits, Monthly Notices of the Royal Astronomical Society, 468(2): 2265-2282, 2017.
[16].Yi Qi, Shijie Xu, Rui Qi*. Transfer from Earth to libration point orbit using lunar gravity assist, Acta Astronautica, 133: 145-157, 2017.
[17].Shuge Zhao, Rui Qi*, Jingrui Zhang, Kaiheng Xiang, Chen Zhang, Jin Jin. Problem A of 9th China trajectory optimization competition: problem description and summary of the results, Acta Astronautica, 150: 178-181, 2018.
[18].Shuge Zhao, Jingrui Zhang, Kaiheng Xiang, Rui Qi. Target sequence optimization for multiple debris rendezvous using low thrust based on characteristics of SSO. Astrodynamics, 1(1): 85-99, 2017.
