Jing Liu, Zelong Chen, Dantong Ge, Shengying Zhu, Pingyuan Cui (2026). Relative Information Assisted Autonomous Navigation for Flexible Landing on Asteroids. IEEE Transactions on Aerospace and Electronic Systems.DOI
Zelong Chen, Pingyuan Cui, Dantong Ge, Shengying Zhu, Shisheng Cui (2026). Unbiased Minimum-Variance Filter for Flexible Landing With Mixed State Constraints. IEEE Transactions on Aerospace and Electronic Systems.DOI
Pingyuan Cui, Zelong Chen, Shengying Zhu, Jiateng Long (2025). Residual learning method for Mars aerobraking autonomous predictive guidance. Aerospace Science and Technology.DOI
Xujin Leng, Shengying Zhu, Pingyuan Cui, Dantong Ge (2025). Multi-Information Assisted Optical Navigation Method for Mars Aerobraking. China Automation Congress (CAC).DOI
Pingyuan Cui, Zelong Chen, Dantong Ge, Shengying Zhu, Shisheng Cui (2024). State Estimation With Nonlinear Inequality Constraints for Small Celestial Body Flexible Landing. IEEE Transactions on Aerospace and Electronic Systems.DOI
Pingyuan Cui, Dongyue Zhao, Zelong Chen, Dantong Ge, Jiateng Long (2024). Intelligent cooperative control for flexible landing on small celestial bodies. Advances in Space Research.DOI
Pingyuan Cui, Chengyu Zhang, Zixuan Liang (2024). Optimal attitude control for landing on asteroid with a flexible lander. Aerospace Science and Technology.DOI
Wenbo Xiu, Jiateng Long, Dantong Ge, Pingyuan Cui, Shengying Zhu (2024). Observability-Based Orbiter Aided Cooperative Navigation for Asteroid Landing.DOI
Pingyuan Cui, Chengyu Zhang, Zixuan Liang (2022). Closed-Loop Guidance for Asteroid Landing Using Stability-Related Control and Three-Dimensional Convex Curvature Constraints. IEEE Transactions on Aerospace and Electronic Systems.DOI
Pingyuan Cui, Dongyue Zhao, Shengying Zhu (2022). Obstacle avoidance guidance for planetary landing using convex trajectory and adaptive curvature regulation. Acta Astronautica.DOI
Yuanqing Xia, Cui Zhu, Pingyuan Cui, Zirui Xing, Li Dai, Liansheng Wang (2022). Mars entry navigation under biases based on adaptive Huber divided difference filter. International Journal of Adaptive Control and Signal Processing.DOI
Jiateng Long, Pingyuan Cui, Shengying Zhu (2022). Vector Trajectory Method for Obstacle Avoidance Constrained Planetary Landing Trajectory Optimization. IEEE Transactions on Aerospace and Electronic Systems.DOI
Shengying Zhu, He Yang, Pingyuan Cui, Rui Lin Xu, Zixuan Liang (2021). Anti-collision zone division based hazard avoidance guidance for asteroid landing with constant thrust. Acta Astronautica.DOI
Dantong Ge, Pingyuan Cui (2021). Collision Risk-Perceptive Landing Control for Small-Body Missions. IEEE Transactions on Aerospace and Electronic Systems.DOI
Pingyuan Cui, Dantong Ge, Shengying Zhu, DongYue ZHAO (2020). Research progress of autonomous planetary landing site assessment and selection. Scientia Sinica Technologica.DOI
Jiateng Long, Shengying Zhu, Pingyuan Cui, Zixuan Liang (2020). Barrier Lyapunov function based sliding mode control for Mars atmospheric entry trajectory tracking with input saturation constraint. Aerospace Science and Technology.DOI
Shengying Zhu, Yi Xiu, Ning Zhang, Rui Lin Xu, Pingyuan Cui (2020). Crater-based attitude and position estimation for planetary exploration with weighted measurement uncertainty. Acta Astronautica.DOI
Pingyuan Cui, Xizhen Gao, Shengying Zhu, Wei Shao (2020). Visual navigation based on curve matching for planetary landing in unknown environments. Acta Astronautica.DOI
He Jia, Shengying Zhu, Pingyuan Cui (2019). Observability-Based Navigation Using Optical and Radiometric Measurements for Asteroid Proximity. IEEE Transactions on Aerospace and Electronic Systems.DOI
Hao Jin, Rui Lin Xu, Pingyuan Cui, Shengying Zhu, Huiping Jiang, Zhou Feng (2019). Heuristic search via graphical structure in temporal interval-based planning for deep space exploration. Acta Astronautica.DOI
Pingyuan Cui, Dantong Ge, He Jia, Shengying Zhu (2019). Prudent small celestial body landing strategy with risk precautions. Acta Astronautica.DOI
Dantong Ge, Pingyuan Cui, Shengying Zhu (2019). Recent development of autonomous GNC technologies for small celestial body descent and landing. Progress in Aerospace Sciences.DOI
Jiateng Long, Ai Gao, Pingyuan Cui, Yang Liu (2018). Mars atmospheric entry guidance for optimal terminal altitude. Acta Astronautica.DOI
Shengying Zhu, Dongchen Liu, Yang Liu, Pingyuan Cui (2018). Observability-based visual navigation using landmarks measuring angle for pinpoint landing. Acta Astronautica.DOI
Zhaoyu Li, Rui Lin Xu, Pingyuan Cui, Shengying Zhu (2018). Correction to: Artificial Neural Network Based Mission Planning Mechanism for Spacecraft. International Journal of Aeronautical and Space Sciences.DOI
Rui Lin Xu, Hao Jin, Wenming Xu, Pingyuan Cui, Xiaodong Han (2018). Effective search strategy via internal state transition graphs on onboard planning for deep space probes. Acta Astronautica.DOI
Pingyuan Cui, Tong Qin, Shengying Zhu, Yang Liu, Rui Lin Xu, Zhengshi Yu (2018). Trajectory curvature guidance for Mars landings in hazardous terrains. Automatica.DOI
Shuo Wang, Pingyuan Cui (2018). Autonomous orbit determination using pulsars and inter-satellite ranging for Mars orbiters. Proceedings - IEEE Aerospace Conference.DOI
Tong Qin, Shengying Zhu, Pingyuan Cui, Enjie Luan (2018). Divert capability analysis and subsequent guidance design for mars landing. Proceedings - IEEE Aerospace Conference.DOI
Yuan Xu, Shengying Zhu, Zhengshi Yu, Pingyuan Cui (2018). Hazard avoidance guidance for planetary landing using a dynamic safety margin index. Proceedings - IEEE Aerospace Conference.DOI
Zeduan Zhao, Zhengshi Yu, Pingyuan Cui (2018). An analytical Mars entry guidance method for higher deployment altitude considering uncertainties. Proceedings - IEEE Aerospace Conference.DOI
Pingyuan Cui, Zeduan Zhao, Zhengshi Yu, Juan Dai (2018). Terminal altitude maximization for Mars entry considering uncertainties. Acta Astronautica.DOI
Dantong Ge, Pingyuan Cui (2018). Extended State Observer-Based Model Predictive Control in Mars Powered Descent. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Jiateng Long, Yang Liu, Pingyuan Cui, Ai Gao (2018). Predictor-Corrector Strategy Based Energy Suboptimal Obstacle Avoidance for Landing on Small Bodies. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Rui Lin Xu, Hui Wang, Wenming Xu, Pingyuan Cui, Shengying Zhu (2017). Rotational-path decomposition based recursive planning for spacecraft attitude reorientation. Acta Astronautica.DOI
Xiao Wei Jiang, Rui Xu, Pingyuan Cui (2017). A heuristic constraint programmed planner for deep space exploration problems.DOI
Hao Jin, Rui Lin Xu, Wenming Xu, Pingyuan Cui, Shengying Zhu (2017). Enriching mission planning approach with state transition graph heuristics for deep space exploration.DOI
Jianfeng Deng, Ai Gao, Hua Zong, Pingyuan Cui (2017). An innovative navigation scheme for Mars entry using dynamic pressure measurement. Advances in Space Research.DOI
Zhengshi Yu, Pingyuan Cui, John L. Crassidis (2017). Design and optimization of navigation and guidance techniques for Mars pinpoint landing: Review and prospect. Progress in Aerospace Sciences.DOI
Shuo Wang, Pingyuan Cui, Ai Gao, Zhengshi Yu, Menglong Cao (2017). Absolute navigation for Mars final approach using relative measurements of X-ray pulsars and Mars orbiter. Acta Astronautica.DOI
Pingyuan Cui, Yanjie Liu, Zhengshi Yu, Shengying Zhu, Wei Shao (2017). Intelligent landing strategy for the small bodies: from passive bounce to active trajectory control. Acta Astronautica.DOI
Yanjie Liu, Shengying Zhu, Pingyuan Cui, Zhengshi Yu, Hua Zong (2017). Hopping trajectory optimization for surface exploration on small bodies. Advances in Space Research.DOI
Changqing Wu, Rui Lin Xu, Shengying Zhu, Pingyuan Cui (2017). Time-optimal spacecraft attitude maneuver path planning under boundary and pointing constraints. Acta Astronautica.DOI
Zeduan Zhao, Zhengshi Yu, Pingyuan Cui (2016). A beacon configuration optimization method based on Fisher information for Mars atmospheric entry. Acta Astronautica.DOI
Pingyuan Cui, Dantong Ge, Ai Gao (2016). Optimal landing site selection based on safety index during planetary descent. Acta Astronautica.DOI
Haibin Shang, Xiaoyu Wu, Pingyuan Cui (2016). Trajectory exploration within asynchronous binary asteroid systems using refined Lagrangian coherent structures. Celestial Mechanics and Dynamical Astronomy.DOI
Xiao Wei Jiang, Pingyuan Cui, Rui Xu, Ai Gao, Shengying Zhu (2016). An action guided constraint satisfaction technique for planning problem. IEEE International Conference on Cognitive Informatics & Cognitive Computing (ICCI*CC).DOI
Zhengshi Yu, Pingyuan Cui, Maolin Ni (2016). A polynomial chaos based square-root Kalman filter for Mars entry navigation. Aerospace Science and Technology.DOI
Pingyuan Cui, Shuo Wang, Ai Gao, Zhengshi Yu (2016). X-ray pulsars/Doppler integrated navigation for Mars final approach. Advances in Space Research.DOI
Zhengshi Yu, Zeduan Zhao, Pingyuan Cui (2016). An Observability-Based Trajectory Optimization Considering Disturbance for Atmospheric Entry. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Tong Qin, Shengying Zhu, Pingyuan Cui (2016). Flying Beacon Aided Entry Navigation for Mars Orbiter-Lander Integrated Mission. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Dantong Ge, Ai Gao, Pingyuan Cui (2016). Online Landing Site Selection Considering Maneuverability Constraint during Mars Powered Descent Phase. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Hu Haijing, Shengying Zhu, Pingyuan Cui (2015). Desensitized optimal trajectory for landing on small bodies with reduced landing error. Aerospace Science and Technology.DOI
Hu Haijing, Shengying Zhu, Pingyuan Cui (2015). Obstacles constrained Mars powered descent trajectory optimization via navigation function. IEEE International Conference on Information and Automation (ICIA).DOI
Zhengshi Yu, Shengying Zhu, Pingyuan Cui, Lina Wang (2015). A robust Kalman filter for mars entry navigation. Chinese Control Conference (CCC).DOI
Jiateng Long, Ai Gao, Pingyuan Cui (2015). Controllable set analysis for planetary landing under model uncertainties. Advances in Space Research.DOI
Yamin Wang, Dong Qiao, Pingyuan Cui (2015). Design of optimal impulse transfers from the Sun–Earth libration point to asteroid. Advances in Space Research.DOI
Zhengshi Yu, Shengying Zhu, Pingyuan Cui (2015). Orbit optimization of Mars orbiters for entry navigation: From an observability point of view. Acta Astronautica.DOI
Zhengshi Yu, Rui Lin Xu, Pingyuan Cui (2015). A Multi Sensor Based Integrated Navigation for Pin-Point Landing on Mars. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Fanyu Zhao, Rui Lin Xu, Pingyuan Cui (2015). Observation Scheduling Problem for Multi-task with Complex Constraints. Communications in computer and information science.DOI
Fanyu Zhao, Pingyuan Cui, Rui Lin Xu, Zhaoyu Li (2014). Attitude navigation for deep space explorer based on mission planning.DOI
Subuda Menggen, Pingyuan Cui, Shengying Zhu (2014). Networked Mars satellite system design and autonomous navigation analysis.DOI
Haibin Shang, Xiaoyu Wu, Pingyuan Cui (2014). Periodic orbits in the doubly synchronous binary asteroid systems and their applications in space missions. Astrophysics and Space Science.DOI
Yamin Wang, Dong Qiao, Pingyuan Cui (2014). Design of low-energy transfer from lunar orbit to asteroid in the Sun-Earth-Moon system. Acta Mechanica Sinica.DOI
Tong Qin, Shengying Zhu, Pingyuan Cui, Ai Gao (2014). An innovative navigation scheme of powered descent phase for Mars pinpoint landing. Advances in Space Research.DOI
Zhengshi Yu, Pingyuan Cui, Shengying Zhu (2014). On the observability of Mars entry navigation using radiometric measurements. Advances in Space Research.DOI
Haning Xiu, Shengying Zhu, Pingyuan Cui (2014). Deep space moving target detection based on technology of image matching.DOI
Yamin Wang, Dong Qiao, Pingyuan Cui (2014). Analysis of Two-Impulse Capture Trajectories into Halo Orbits of Sun–Mars System. Journal of Guidance Control and Dynamics.DOI
Zhengshi Yu, Pingyuan Cui, Shengying Zhu (2014). Observability-Based Beacon Configuration Optimization for Mars Entry Navigation. Journal of Guidance Control and Dynamics.DOI
Haibin Shang, Shuai Wang, Pingyuan Cui (2014). Fast low-energy halo-to-halo transfers between Sun–planet systems. Chinese Journal of Aeronautics.DOI
Pingyuan Cui, Dong Qiao (2014). The present status and prospects in the research of orbital dynamics and control near small celestial bodies*. Theoretical and Applied Mechanics Letters.DOI
Dong Qiao, Pingyuan Cui, Yamin Wang, Jiangchuan Huang, Linzhi Meng, Degang Jie (2013). Design and analysis of an extended mission of CE-2: From lunar orbit to Sun–Earth L2 region. Advances in Space Research.DOI
Xiangyu Li, Dong Qiao, Pingyuan Cui (2013). The equilibria and periodic orbits around a dumbbell-shaped body. Astrophysics and Space Science.DOI
Pingyuan Cui, Zhengshi Yu, Shengying Zhu, Ai Gao (2013). Real-time Navigation for Mars Final Approach Using X-ray Pulsars. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
Zun-Hui Zhao, Haibin Shang, Pingyuan Cui, Shuai Wang (2013). Launch opportunity research for Earth-Mars low thrust trajectory.
Fanyu Zhao, Pingyuan Cui, Rui Lin Xu, Ting Peng, Dexiang Chen (2013). Planner test and analyzing system for deep space mission. International Conference on Control and Automation.DOI
Zunhui Zhao, Haibin Shang, Pingyuan Cui, Xiang‐Yu Huang (2013). Solution space research for interplanetary trajectory. Aircraft Engineering and Aerospace Technology.DOI
Kai Wu, Hutao Cui, Pingyuan Cui (2013). Extended High-Gain Observer for Mars Entry Guidance. TELKOMNIKA Indonesian Journal of Electrical Engineering.DOI
Zunhui Zhao, Haibin Shang, Pingyuan Cui, Xiang‐Yu Huang (2012). Low thrust gravity assist trajectory optimization based on hybrid method. IEEE International Conference on Advanced Computational Intelligence.DOI
Yamin Wang, Pingyuan Cui, Dong Qiao (2012). Opportunities search of transfer between interplanetary halo orbits in ephemeris model. Science China Technological Sciences.DOI
Shengying Zhu, Pingyuan Cui, Hu Haijing (2012). Hazard detection and avoidance for planetary landing based on Lyapunov control method. World Congress on Intelligent Control and Automation.DOI
Zhengshi Yu, Shengying Zhu, Pingyuan Cui (2012). Sequence detection of planetary surface craters from DEM data. World Congress on Intelligent Control and Automation.DOI
Haining Pan, Pingyuan Cui, Huan Wang (2012). Spherical terrain matching for SLAM in planet exploration. World Congress on Intelligent Control and Automation.DOI
Dong Qiao, Pingyuan Cui, Yamin Wang, Jiangchuan Huang, Linzhi Meng, Degang Jie (2012). Design and analysis of an extended mission of CE-2: From lunar orbit to Sun–Earth L2 region. 39th COSPAR Scientific Assembly.
Dong Qiao, Pingyuan Cui, Hutao Cui (2012). Proposal for a multiple-asteroid-flyby mission with sample return. Advances in Space Research.DOI
Pingyuan Cui (2012). Searching Launch Opportunity of Asteroid Exploration from Moon Departure. Journal of Astronautics.
Pingyuan Cui, Ai Gao, Hutao Cui (2012). Receding Horizon-Based Dual Control Strategy for Pinpoint Planetary Landing. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.DOI
Zhenjiang Zhang, Hutao Cui, Pingyuan Cui (2012). Determining Novel Periodic Orbits around Equilibrium Points of Asteroids. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.DOI
Tiezheng Li, Hehua Ju, Pingyuan Cui (2011). Mission Planning Method for Planetary Rover Based on Path Planning. International Conference on Intelligent Human-Machine Systems and Cybernetics.DOI
Jianqing Chen, Pingyuan Cui, Hui-tao Cui (2011). Automated detection and classification for craters based on geometric matching. Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE.DOI
Gaofeng Ren, Hutao Cui, Pingyuan Cui, Enjie Luan (2011). A rapid uncertainty propagation method for pre-parachute phase of Mars entry. Chinese Control and Decision Conference (CCDC).DOI
Pingyuan Cui (2011). Research on Third-Order Analytical Solution Determination of Halo Orbits around Equilibrium Point of Asteroid. Journal of Astronautics.
Pingyuan Cui (2011). Research on the Kinematics and Dynamics of Lunar Rover "BH-1". Journal of Beijing University of Technology.
Zhenjiang Zhang, Hutao Cui, Pingyuan Cui, Yu Meng (2010). Modeling and Analysis of Gravity Field of 433Eros Using Polyhedron Model Method. International Conference on Information Engineering and Computer Science.DOI
Ai Gao, Pingyuan Cui, Hutao Cui (2010). Research on optical/inertial integrated navigation for soft landing on asteroids using mixed H2/H∞ filter. International Conference on Intelligent Control and Information Processing.DOI
Pingyuan Cui, Dong Qiao, Hutao Cui, Enjie Luan (2010). Target selection and transfer trajectories design for exploring asteroid mission. Science China Technological Sciences.DOI
李鹏，崔平远，崔祜涛 (2009). Spacecraft formation control strategy on Sun-Earth Lissajous orbit. Journal of Harbin Institute of Technology(New series).
崔平远，李鹏，崔祜涛 (2009). Motion modeling and formation form analysis of spacecraft near collinear libration points. Journal of Harbin Institute of Technology(New series).
Haining Pan, Zhenwu Lei, Pingyuan Cui, Hehua Ju (2009). Obstacle avoidance learning for a wheeled lunar rover based on its local relative pose.
Yan Ma, Hehua Ju, Pingyuan Cui (2009). Research on Localization and Mapping for Lunar Rover Based on RBPF-SLAM. International Conference on Intelligent Human-Machine Systems and Cybernetics.DOI
Dong Qiao, Hutao Cui, Pingyuan Cui (2009). The design of transfer trajectory for Ivar asteroid exploration mission. Acta Astronautica.DOI
崔平远，尚海滨，任远，栾恩杰 (2008). Optimization of multi-revolution low-thrust transfer based on modified direct method. Journal of Harbin Institute of Technology(New series).