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2016-2020
- Zhu, X. Zhang, H. Gao, Y. Correlations between the scaling factor and fitness values in differential evolution, IEEE Acess, 2020, 8, 32100-32120.
- Wang, W. Shu, L. Liu, J. Gao, Y. Joint navigation performance of distant retrograde orbits and cislunar orbits via LiAISON considering dynamic and clock model errors, Navigation, 2019, 66(4): 781-802.
- Meng Y, Zhang H. Gao Y. Low-Thrust Minimum-Fuel Trajectory Optimization Using Multiple Shooting Augmented by Analytical Derivatives. Journal of Guidance, Control, and Dynamics, 2019, 42(3), 662-677.
- Liu, W. Gao, Y. Dong, W. Li, Z. Flight Test Results of the Microgravity Active Vibration Isolation System in China's Tianzhou-1 Mission. Microgravity Science and Technology, 2018, 30(6), 995–1009.
- 彭超、温昶煊、高扬. 地月空间DRO与HEO(3∶1/2∶1)共振轨道延拓求解及其稳定性分析，载人航天，2018, 24(6):703-718.
- 王彗木,刘伟,高扬.“绳网飞行器＋绳系机械爪”捕获近地小行星的新概念方案.载人航天，2018,24(4):470-478.
- 马剑、孟雅哲、朱小龙、何胜茂、高扬，特定区域密集观测的低轨卫星星座最优设计方法，中国科学-技术科学，2018,048（002), 170-184.
- 朱政帆，高扬，空间小推力轨道最优Bang_Bang控制的两类延拓解法综述，深空探测学报，2017,4(2): 101-110.
- Peng, C. Gao, Y. Formation-Flying Planar Periodic Orbits in the Presence of Inter-satellite Lorentz Force, IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(3): 1412-1430.
- Zhu, Z. Gan, Q. Yang, X. Gao, Y. Solving Fuel-Optimal Low-Thrust Orbital Transfers with Bang-Bang Control Using a Novel Continuation Technique, Acta Astronautica, 2017,137: 98-133.
- He,S. Zhu, Z.Peng C. Ma, J. Zhu, X. Gao, Y, Optimal design of near-Earth asteroid sample-return trajectories in the Sun-Earth-Moon system, Acta Mechanica Sinica, 2016, 28(5): 1466-1478.
2011-2015
- 王文彬、高扬，精密定轨中三类经验加速度的有效建模方法，宇航学报，36（12），2015，755-762。
- 朱小龙、刘迎春、高扬，航天器最优受控绕飞轨迹推力幅值延拓设计方法，力学学报，Vol.46, No.5, 2014, pp.756-769.
- Gao, Y., Analysis of the Earth co-orbital motion of Chang’e-2 after asteroid flyby, Chinese Science Bulletin, Vol. 59, No. 17, 2014. pp.2045-2049.
- Gao, Y., Near-Earth Asteroid Flyby Trajectories from the Sun-Earth L2 for Chang’e-2’s Extended Flight. Acta Mechanica Sinica. Vol. 29, No.1, 2013, pp.123-131.
- Gao, Y., Li, H., He, S. First-round Design of Flight Scenario for Chang’e-2’s Extended Mission: Taking Off from Lunar Orbit. Acta Mechanica Sinica, Vol.28, No.5, 2012. pp.1466-1478.
- 彭超、高扬，近圆参考轨道卫星编队洛仑兹力控制，《力学学报》，V44(5), 851-860, 2012.（入选庆祝《力学学报》创刊55周年专栏）
- 何胜茂、谭高威、高扬，第三届深空轨道设计竞赛冠军团队方法与结果，《力学与实践》，Vol.34, No.3, 2012. pp.95-101.
- Peng, C., Gao, Y., Lorentz-Force-Perturbed Orbits with Application to J2-Invariant Formation. Acta Astronautica, Vol.77, 2012, pp.12-28.
- 高扬，电火箭星际航行：技术进展、轨道设计与综合优化，《力学学报》，Vol.43, No.6, 2011. pp. 991-1019.（纪念力学学报首任主编钱学森诞辰100周年专栏约稿）
2006-2010
- Gao, Y., Li. X., Optimization of Low-Thrust Many-Revolution Transfers and Lyapunov-based Guidance, Acta Astronautica, Vol.66, Nos.1~2, 2010, pp.117-129.
- Gao, Y., Linear Feedback Guidance for Low-Thrust Many-Revolution Earth-Orbit Transfers, Journal of Spacecraft and Rockets, Vol.46, No. 6, 2009, pp. 1320-1325.
- Gao, Y., Li, W., Systematic Direct Approach for Optimizing Continuous-Thrust Earth-Orbit Transfers, Chinese Journal of Aeronautics, Vol.29, No. 1, 2009, pp.56-69.
- Gao, Y., Direct Optimization of Low-Thrust Many-Revolution Orbital Transfers, Chinese Journal of Aeronautics, Vol. 22, No. 4, pp. 426-433, 2009.
- Gao, Y., Low-Thrust Nonlinear Guidance by Tracking Mean Orbital Elements, Journal of Guidance, Control, and Dynamics, Vol.31, No.4, 2008, pp. 1103-1110.
- Gao, Y., Near-Optimal Very Low-Thrust Earth-Orbit Transfers and Guidance Schemes, Journal of Guidance, Control, and Dynamics, Vol.30, No.2, 2007, pp.529-539.
- Gao, Y., Low-Thrust Interplanetary Transfers Including Escape and Capture Trajectories, Journal of Guidance, Control, and Dynamics, Vol.30, No.6, 2007, pp. 1814-1818.
- Gao, Y., Earth-Moon Trajectory Optimization Using Solar Electric Propulsion, Chinese Journal of Aeronautics, Vol.20, No.5, 2007, pp.452-463.
2001-2005
- Gao, Y., Kluever, C. A., Engine-Switching Strategies for Interplanetary Solar Electric Propulsion Spacecraft, Journal of Spacecraft and Rockets, Vol.42, No.4, 2005, 765-767.
- Gao, Y., Kluever, C. A., Analytic Orbital Averaging Technique for Computing Tangential-Thrust Trajectories, Journal of Guidance, Control, and Dynamics, Vol. 28, No.6, 2005, pp.1320-1323.
- Gao, Y., Kluever, C. A., Low-Thrust Guidance Scheme for Earth-Capture Trajectories, Journal of Guidance, Control, and Dynamics, Vol.28, No.2, 2005, pp.333-342.
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