近期论文
查看导师最新文章
（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）
陈 正,崔祜涛,田 阳,饶 炜,董 捷. 天问一号着陆器大底分离安全性分析与验证.宇航学报. 2022,43(1):81-90
陈 正，崔祜涛，田 阳，黄翔宇. 天问一号着陆器 EDL 过程建模与仿真. 宇航学报. 2022,43(1):91-102
Zhang, Yingying Huang, Jiangchuan Cui, Hutao. Trajectory Design via Convex Optimization for Six-Degree-of-Freedom Asteroid Powered Landing. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS. 2021,44(4):779-792
Zhang, Yingying Huang, Jiangchuan Cui, Hutao.Trajectory optimization for asteroid landing with two-phase free final time.ADVANCES IN SPACE RESEARCH.2020,65(4):1210-1224
Yao, MB ; Belke, CH ; Cui, HT; Paik, J.A reconfiguration strategy for modular robots using origami folding INTERNATIONAL JOURNAL OF ROBOTICS RESEARCH. Volume: 38 Issue: 1 Pages: 73-89
Xiao, XM , Yao, MB ,Cui, HT*,Fu, YG. Safe Mars landing strategy: Towards lidar-based high altitude hazard detection. ADVANCES IN SPACE RESEARCH. 2019, 63 (8): 2535-2550
Zheng Yiyu, Cui Hutao, Ai Yuanhang. Indirect Trajectory Optimization for Mars Entry with Maximum Terminal Altitude. JOURNAL OF SPACECRAFT AND ROCKETS. 2017. 54( 5): 1068-1080
Ai, YH ,Cui, HT * , Zheng, YY. Identifying method of entry and exit conditions for aerocapture with near minimum fuel consumption. AEROSPACE SCIENCE AND TECHNOLOGY. 2016, 58: 582-593
Zheng Yiyu, Cui Hutao *. Mars Atmospheric Entry Guidance Using a Sensitivity Method. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS. 2017, 53(4): 1672-1684
Xiao, XM,Cui, HT * ,Yao, MB ,Tian, Y . Autonomous rock detection on mars through region contrast. ADVANCES IN SPACE RESEARCH. 2017, 60 ( 3): 626-635
Li J, Cui H, Tian Y.Nonlinearity analysis of measurement model for vision-based optical navigationsystem[J]. Acta Astronautica, 2015, 107:70–78.
Yiyu Zheng, Hutao Cui, andYuanhang Ai. Constrained Numerical Predictor–Corrector Guidance for Mars PrecisionLanding. JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS. 2017,40(1): 177-185
Xiao X, Cui H, Tian Y. Robustplane fitting algorithm for landing hazard detection[J]. IEEE Transactions onAerospace & Electronic Systems, 2015, 51(4):2864-2875.
Zheng Y, Cui H. Disturbanceobserver-based robust guidance for Mars atmospheric entry with inputsaturation[J]. Chinese Journal of Aeronautics, 2015, 28(3): 845-852.
Yu M, Cui H. Robust hazardmatching approach for visual navigation application in planetary landing[J].Aerospace Science & Technology, 2015, 47:378-387.
Zheng Y, Cui H, Tian Y.Improvements to Entry Terminal Point Controller for Mars Atmospheric Entry[C]//AIAA Atmospheric Flight Mechanics Conference, 2015.
Zheng Y, Cui H. Optimalnonlinear feedback guidance algorithm for Mars powered descent[J]. AerospaceScience & Technology, 2015, 45:359-366.
Yu M, Cui H, Tian Y. A newapproach based on crater detection and matching for visual navigation inplanetary landing[J]. Advances in Space Research, 2014, 53(12):1810-1821.
Cui Hutao, Cheng Xiaojun.Anti-unwinding attitude maneuver control of spacecraft considering boundeddisturbance and input saturation, SCIENCE CHINA-TECHNOLOGICALSCIENCES,2012,55(9): 2518-2529
Zhang Zhenjiang, Cui Hutao, CuiPingyuan. Determining Novel Periodic Orbits around Equilibrium Points ofAsteroids. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACESCIENCES,2012,55(1):44-50
Qiao Dong, Cui Hutao, CuiPingyuan. The design of transfer trajectory for Ivar asteroid explorationmission. Acta Astronautica. 2009, 65(11-12): 1553-1560.
Qiao Dong, Cui Hutao, CuiPingyuan. Evaluating Accessibility of Near-Earth Asteroids Via Earth GravityAssists. Journal of Guidance, Control, and Dynamics. 2006, 29(2):502-505
Huang Xiangyu, Cui Hutao, CuiPingyuan. An autonomous optical navigation and guidance for soft landing onasteroids. Acta Astronautica. May, 2004, 54 (10): 763-771
Li Shuang, Cui Pingyuan and CuiHutao. Vision-aided Inertial Navigation for Pinpoint Planetary Landing.Aerospace Science and Technology. 2007, 11(6): 499-506 (SCI: 199WN, EI:072910705103)
Li Shuang, Cui Pingyuan and CuiHutao. Autonomous navigation and guidance for landing on asteroids. AerospaceScience and Technology. 2006, 10(3): 239-247 (SCI: 037GP (IDS Number) EI: 06189847701)
Li, Shuang, Cui, Hutao; Cui,Pingyuan Autonomous optical navigation for landing on asteroids. AircraftEngineering and Aerospace Technology, 2005, 77(4): 317-323(EI: 05329281395)(SCI, IDS Number: 956IG)[April, 2005. United Kingdom]
Li Peng, Cui Pingyuan, CuiHutao. An improved nonlinear control strategy for deep space formation flyingspacecraft. Acta Mechanica Sinica. 2009, 25(6): 847-856 (SCI: 522RS)
Qiao Dong, Cui Pingyuan, CuiHutao. Target Selection and Accessibility for Rendezvous with Near-EarthAsteroid Mission. Earth, Moon and Planets. 2007, 100(3-4): 137-156 (SCI: 171JN,EI: 94051276645)
Li Peng, Cui Hutao, CuiPingyuan. UPF based Autonomous Navigation Scheme for Deep Space Probe. Journalof Systems Engineering and Electronics. 2008, 19(3): 529-536 (SCI: 322XF, EI:082711349953)
Huang, Xiangyu, Cui, Hutao;Cui, Pingyuan; Luan, Enjie. Autonomous orbit determination for the probe aroundsmall body. Journal of Systems Engineering and Electronics. September, 2004,15(3): 327-332（EI: 04518734342）
CUI Ping-yuan, CUI Hu-tao,HUANG Xiang-yu, LUAN En-jie. Autonomous determination of orbit for probe aroundasteroids using unscented Kalman filter. Journal of Harbin Institute ofTechnology. 2003, 10(3): 229-234（EI: 04208164513）
CUI Hu-tao, QIAO Dong, CUIPing-yuan, LUAN En-jie. Design of MGA trajectories for main belt asteroid.Journal of Harbin Institute of Technology. 2003, 10(4): 443-446（EI:04198148840）
CUI Hu-tao, CUI Ping-yuan, LUANEn-jie. Impulsive orbit control for spacecraft around asteroid. Journal ofHarbin Institute of Technology. 2003, 10(4): 349-352（EI: 04188147583）
冯军华，崔祜涛，崔平远. 行星表面陨石坑检测与匹配方法, 航空学报,2010,31(9):1858-1863 (EI: 20104313323756)
朱圣英，崔祜涛, 崔平远. 基于路标信息的绕飞小天体探测器自主光学导航方法研究, 电子学报,2010,38(9):2052-2058 (EI: 20104713408775)
朱圣英 , 崔平远 , 崔祜涛 , 邵巍. 基于路标观测角的星际着陆器自主位姿确定技术, 航空学报, 2010, 31(2):318-326
常晓华,崔平远,崔祜涛. 基于太阳观测的深空巡航段自主导航方法研究,宇航学报, 2010, 31(4): 1017-1023(EI: 20102413003054)
田阳,崔平远,崔祜涛. 基于图像的着陆点评估及探测器运动估计方法,宇航学报, 2010,31(1): 98-103(EI: 20101412827445)
王晓明，崔祜涛，崔平远，线性系统观测性的鲁棒性. 吉林大学学报，2009，39（s1）：286-290（EI：20091912073524）
徐田来,崔平远,崔祜涛. 路网辅助的车载INS/GPS组合导航方法研究. 控制与决策. 2009,24(3): 398-402
田阳，崔平远，崔祜涛，基于图像序列的软着陆小天体自主导航方法. 宇航学报, 2009,30(1): 210- 214
常晓华，崔祜涛，崔平远， 刘宇飞; 一种基于视线矢量的双星系统自主导航方法研究. 系统仿真学报，2009，21（13）：4088-4096
刘宇飞, 崔平远, 崔祜涛. 深空导航系统状态描述形式的选取问题研究. 宇航学报. 2008, 29(1): 115-120(EI: 20084911768169)
邵巍, 崔平远, 崔祜涛. 一种基于形态学的探测器安全着陆点选择方法. 宇航学报. 2008, 29(2): 659-664(EI: 20084911768265)
崔祜涛, 骆军红, 崔平远, 冯军华. 基于控制杆的太阳帆姿态控制研究. 宇航学报. 2008, 29(2): 560-566(EI: 20084911768247)
徐文明, 崔祜涛, 崔平远, 刘宇飞. 深空自主光学导航小行星筛选与规划方法研究. 航空学报. 2007, 28(4): 891-896 (EI: 073410777250)
臧荣春, 崔平远, 崔祜涛, 金艺. 基于IMM-UKF的组合导航算法. 控制理论与应用. 2007, 24(4): 634-638 (EI: 074110859670)
岳富占, 崔平远, 崔祜涛. 基于视觉序列图像的月球车自运动估计技术. 系统仿真学报. 2007, 19(13): 3033-3037 (EI: 073010707627)
李鹏, 崔祜涛, 崔平远. 探测器交会小天体的UPF自主导航方案. 吉林大学学报(工学版). 2007, 37(3): 691-695 (EI: 072410652672)
李爽, 崔祜涛, 崔平远. 着陆小天体的自主GNC技术研究. 宇航学报, 2006, 27(1): 21-26 (EI: 06209881919)
徐田来, 崔平远, 崔祜涛. 基于置信度加权的组合导航数据融合算法研究. 航空学报, 2007, 28(6):1389-1394
岳富占, 崔平远, 崔祜涛, 居鹤华. 月球巡视探测器自主定向算法研究. 航空学报. 2006, 27(3): 500-504（EI: 062910014226）
仲维国, 崔祜涛, 崔平远. 三轴稳定深空探测器的自主姿态制导. 宇航学报. 2006, 27(2): 286-290 (EI: 06289996545)
岳富占, 崔平远, 崔祜涛, 居鹤华. 基于地球敏感器和加速度计的月球车自主定向算法研究. 宇航学报. 2005, 26(5): 553-557（EI: 05499528638）
崔祜涛, 史雪岩, 崔平远, 栾恩杰. 绕飞慢自旋小天体的航天器运动分析. 航空学报. 2004, 25(1): 16-20（EI: 04218172266）
崔祜涛, 史雪岩, 崔平远, 栾恩杰. 航天器环绕小行星Ivar的运动分析.宇航学报. 2004, 25(3): 251-255（EI: 04398379111）
黄翔宇, 崔平远, 崔祜涛, 栾恩杰. 利用Gauss-Markov过程的着陆小天体导航与制导方法. 宇航学报. 2004, 25(3): 338-342
黄翔宇, 崔祜涛, 崔平远. 探测器着陆小天体的自主光学导航研究. 电子学报. 2003, 31(5): 659-661（EI: 03367625543）
崔祜涛，崔平远. 软着陆小行星的自主导航与制导. 宇航学报,2002, 23(5):1-4 (EI:03187454279)
京公网安备 11010802027423号