[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]崔平遠, 龍嘉騰*, 朱聖英等. 行星着陸軌迹優化技術研究進展[J]. 宇航學報, 2021, 42(6): 100-109.
[9]龍嘉騰, 葛丹桐, 崔平遠*. 火星精确着陸軌迹優化與制導技術研究進展[J]. 航天返回與遙感, 2021, 42(3): 13-22.
[10]龍嘉騰, 高艾,崔平遠*. 火星大氣進入段側向預測校正制導律設計[J]. 深空探測學報,2016, 3(2):145-149.