[1] Pingyuan Cui, Xizhen Gao, Shengying Zhu*. Visual Navigation Based on Curve Matching for Planetary Landing in Unknown Environments. Acta Astronautica. 2020,170: 261-274
[2]崔平远，秦同，朱圣英，火星动力下降自主导航与制导技术研究进展，宇航学报，2020，41(1) : 1-9
[3]Pingyuan Cui, Dantong Ge, He Jia, Shengying Zhu*. Prudent Small Celestial Body Landing Strategy with Risk Precautions. Acta Astronautica. 2019,165: 259-267
[4]Dantong Ge, Pingyuan Cui*, Shengying Zhu. Recent Development of Autonomous GNC Technologies in Small Celestial Body Descent and Landing. Progress in Aerospace Sciences. 2019, 110: 100551
[5]赵泽端，崔平远，朱圣英，火星大气进入段纵向可达区生成的解析同伦法，宇航学报，2019，40(9) : 1024-1033
[6]崔平远，赵泽端，朱圣英，火星大气进入段轨迹优化与制导技术研究进展，宇航学报，2019，40(6) : 611-620
[7]Pingyuan Cui, Tong Qin, Shengying Zhu, Yang Liu, Rui Xu*, Zhengshi Yu. Trajectory Curvature Guidance for Mars Landing in Hazardous Terrains. Automatica. 2018, 93: 161-171
[8] Pingyuan Cui, Xizhen Gao, Shengying Zhu*. Visual navigation using edge curve matching for pin-point planetary landing. Acta Astronautica. 2018, 146: 171-180
[9] Pingyuan Cui, Zeduan Zhao, Zhengshi Yu*, Juan Dai. Terminal Altitude Maximization for Mars Entry Considering Uncertainties. Acta Astronautica. 2018, 145: 446-455
[10] Zhengshi Yu, Pingyuan Cui*, John L Crassidis. Design and Optimization of Navigation and Guidance Techniques for Mars Pinpoint Landing: Review and Prospect. Progress in Aerospace Sciences. 2017, 94: 82-94
[11] Shuo Wang, Pingyuan Cui, Ai Gao*, Zhengshi Yu. Absolute Navigation for Mars Final Approach using Relative measurements of X-ray pulsars and Mars orbiter. Acta Astronautica. 2017, 138: 68-78
[12] Pingyuan Cui, Yanjie Liu, Zhengshi Yu*, Shengying Zhu. Intelligent Landing Strategy for the Small Bodies: from Passive Bounce to Active Trajectory Control. Acta Astronautica. 2017, 137: 232-242
[13] Pingyuan Cui, Dantong Ge, Ai Gao*. Optimal landing site selection based on safety index during planetary descent. Acta Astronautica. 2017, 132: 326-336
[14] 葛丹桐，崔平远*，高艾，火星安全着陆轨迹快速生成的能控集法，宇航学报， 2017，38(5) : 497-505
[15] Pingyuan Cui, Shuo Wang, Ai Gao*, Zhengshi Yu. X-Ray Pulsars/Doppler Integrated Navigation for Mars Final Approach. Advances in Space Research. 2016, 57(9): 1889-1900
[16] Yu Zhengshi, Cui Pingyuan*, Ni Maolin. A Polynomial Chaos Based Square-root Kalman Filter for Mars Entry Navigation. Aerospace Science and Technology. 2016,51:192–202
[17] 崔平远，袁旭等，小天体自主附着技术研究进展 ，宇航学报， 2016，37(7) : 759-767
[18] Yu Zhengshi, Cui Pingyuan*, Zhu Shengying. Observability based Beacon Configuration Optimization for Mars Entry Navigation. Journal of Guidance, Control, and Dynamics. 2015, 38(4): 643-650
[19] Long, Jiateng; Gao, Ai; Cui, Pingyuan*. Controllable set analysis for planetary landing under model uncertainties. Advances in Space Research. 2015, 56(2): 281-292
[20] 崔平远，胡海静，朱圣英，火星精确着陆制导问题分析与展望，宇航学报，2014，35(3): 245-253
[21]崔平远, 徐瑞, 朱圣英，赵凡宇. 深空探测器自主技术发展现状与趋势. 航空学报. 2014, 35(1): 13-28
[22] 崔平远, 于正湜, 朱圣英. 火星进入段自主导航技术研究现状与展望. 宇航学报. 2013, 34(4): 447-456
