[1]岳宝增. 液体大幅晃动动力学. 北京, 科学出版社, 30万字, 2011
[2]Liu Feng, Yue Baozeng, Arun K. Banerjee, et al.. Large Motion Dynamics of In-Orbit Flexible Spacecraft with Large Amplitude Propellant Slosh, Journal of Guidance, Control, and Dynamics, 2020, 43(3): 438-450
[3]Xu Yanli, Yue Baozeng, Yang Shuxing. Study on the chaotic dynamics in yaw-pitch-roll coupling of asymmetric rolling projectiles with nonlinear aerodynamics, Nonlinear Dynamics, 2019, 97(4): 2739-2756
[4]Liu Feng, Yue Baozeng. 3DOF-rigid-pendulum analogy for nonlinear liquid slosh in spherical propellant tanks, Journal of Sound and Vibration, 2019, 460: 114907
[5]Tang Yong, Yue Baozeng. Improved method for implementing contact angle condition in simulation of liquid sloshing under microgravity, International Journal for Numerical Methods in Fluids, 2019, 89(4-5): 123-142, 2019.
[6]Tang Yong, Yue Baozeng. Simulation of Large-Amplitude Three-Dimensional Liquid Sloshing in Spherical Tanks, AIAA Journal, 2017, 55(6): 1-8
[7]Liu Feng, Yue Baozeng. Attitude dynamics and control of spacecraft with a partially filled liquid tank and flexible panels. Acta Astronautica, 2018, 143: 327-336
[8]Deng Mingle, Yue Baozeng. Attitude Tracking Control of flexible spacecraft with large amplitude slosh. Acta Mechanica Sinica, 2017, 133: 111-120
[9] Yue Baozeng, Wu Wenjun. Modeling and Coupling Dynamics of the Spacecraft with Multiple Propellant Tanks. AIAA Journal, 2016, 54(11): 3608-3618
[10] Deng Mingle, Yue Baozeng. Position and attitude control of a spacecraft with large amplitude propellant slosh and depletion, Journal of Aerospace Engineering, 2017, 30(6): 1943-5525.0000636
[11] Yan Yulong, Yue Baozeng. Dynamic analysis of the flexible spacecraft with liquid sloshing in axisymmetrical container, Journal of Spacecraft and Rocket, 2018, 55: 282-291
[12] Deng Mingle, Yue Baozeng. Attitude Tracking Control of flexible spacecraft with large amplitude slosh. Acta Mechanica Sinica, 2017,133: 111-120
[13]岳宝增,于嘉瑞.多储液腔航天器刚液耦合动力学与复合控制. 力学学报, 2017, 49(2): 390-396
[14]刘峰,岳宝增.多充液贮腔航天器耦合动力学与姿态控制.宇航学报,2020,41(1):10-17
[15]岳宝增,李晓玉.航天器平移及姿态机动自适应终端滑模控制.动力学与控制学报,2018,16(4):332-337
[16]岳宝增, 宋晓娟. 具有刚-柔-液-控耦合的航天器动力学研究进展.力学进展, 2013, 43(1): 686-696
