[1]Jiateng Long, Fen Wu*. Iterative-Learning-Control-Based Tracking for Asteroid Close Proximity Operation[J]. Journal of Guidance, Control, and Dynamics. 2019, 42(5): 1195-1203.
[2]Jiateng Long, Pingyuan Cui*, Shengying Zhu. Vector Trajectory Method for Obstacle Avoidance Constrained Planetary Landing Trajectory Optimization[J]. IEEE Transactions on Aerospace and Electronic Systems. 2022, 58(4): 2996-3010.
[3]Zelong Chen, Jiateng Long*, Pingyuan Cui. Trajectory Design for Landing on Small Celestial Body with Flexible Lander[J]. Acta Astronautica. 2023, 212: 492-504.
[4]Jiateng Long, Ai Gao, Pingyuan Cui*, et al. Mars Atmospheric Entry Guidance for Optimal Terminal Altitude[J]. Acta Astronautica. 2019, 155: 274-286.
[5]Jiateng Long, Shengying Zhu*, Pingyuan Cui, et al . Barrier Lyapunov Function Based Sliding Mode Control for Mars Atmospheric Entry Trajectory Tracking with Input Saturation Constraint[J]. Aerospace Science and Technology. 2020, 106: 106213.
[6]Jiateng Long, Shengying Zhu*, Zixuan Liang, et al. Rapid Generation of the Fuel-Optimal Trajectory for Landing on Irregularly Shaped Asteroids[J]. IEEE Transactions on Aerospace and Electronic Systems; 57(6): 4390-4400.
[7]Jiateng Long, Ai Gao, Pingyuan Cui*. Controllable Set Analysis for Planetary Landing under Model Uncertainties[J]. Advances in Space Research, 2015, 33(2):281-292.
[8]崔平远, 龙嘉腾*, 朱圣英等. 行星着陆轨迹优化技术研究进展[J]. 宇航学报, 2021, 42(6): 100-109.
[9]龙嘉腾, 葛丹桐, 崔平远*. 火星精确着陆轨迹优化与制导技术研究进展[J]. 航天返回与遥感, 2021, 42(3): 13-22.
[10]龙嘉腾, 高艾，崔平远*. 火星大气进入段侧向预测校正制导律设计[J]. 深空探测学报，2016, 3(2):145-149.
