RBF NN-Based Backstepping Control for Strict Feedback Block Nonlinear System and Its Application. - Yunan Hu; Yuqiang Jin; Pingyuan Cui (ISNN (2), 2004)

Fuzzy Output Tracking Control and Its Application to Guidance Control for Lunar Gravity-Turn. - Pingyuan Cui; Junwei Sun; Fengqiu Liu (ICMLC, 2005)

Sliding Mode Control for Uncertain Nonlinear Systems Using RBF Neural Networks. - Xu Zha; Pingyuan Cui (ISNN (3), 2005)

Realization of multi-agent planning system for autonomous spacecraft. - Rui Xu; Pingyuan Cui; Xiaofei Xu (Adv. Eng. Softw., 2005)

Stabilizing Second-Order Linear Dynamic Systems Via Hybrid Output Feedback Controls. - Liguo Zhang; Yangzhou Chen; Pingyuan Cui (International Conference on Computational Science (2), 2006)

An Innovation Filtering Multiple Model Algorithm for Integrated Navigation System. - Rong-chun Zang; Pingyuan Cui (ICICIC (3), 2006)

Research on Autonomous Navigation of Lunar Rovers for the Moon Exploration. - Pingyuan Cui; Fuzhan Yue; Hutao Cui (ROBIO, 2006)

Recovery of Egomotion from Optical Flow with Large Motion Based on Subspace Method. - Zexu Zhang; Pingyuan Cui; Hutao Cui (ROBIO, 2006)

An Iterative Uniformly Ultimate Boundedness Control Method for Uncertain Switched Linear Systems. - Liguo Zhang; Yangzhou Chen; Pingyuan Cui (ICCSA (1), 2007)

Analyzing and designing of lunar rover motion controller. - Rui Xu; Huiping Jiang; Shengjing Tang; Pingyuan Cui; Fuzhan Yue (ROBIO, 2007)

Guaranteed Cost Control for uncertain discrete-Time delayed Systems: a delay-dependent Approach. - Liguo Zhang; Yangzhou Chen; Pingyuan Cui (Control. Intell. Syst., 2007)

Traction Control on Loose Soil for a Redundantly Actuated Mobile Robot. - Zhenwu Lei; Pingyuan Cui; Hehua Ju; Xingwen Peng (ICIRA (1), 2008)

Lunar Rover's Behavior Fusion Learning Based on Nonholonomic Dynamics. - Haining Pan; Pingyuan Cui; Hehua Ju (ICIRA (1), 2008)

Safe Landing Site Selection Based on Computational Geometry and Genetic Algorithm. - Wei Shao; Pingyuan Cui; Weiwen Zhou (ICNC (1), 2008)

Robust sliding mode guidance and control for soft landing on small bodies. - Zexu Zhang; Weidong Wang; Litao Liang; Xiangyu Huang; Hutao Cui; Shuang Li 004; Pingyuan Cui (J. Frankl. Inst., 2012)

Planner test and analyzing system for deep space mission. - Fanyu Zhao; Pingyuan Cui; Rui Xu; Ting Peng; Dexiang Chen (ICCA, 2013)

Observation Scheduling Problem for Multi-task with Complex Constraints. - Fanyu Zhao; Rui Xu; Pingyuan Cui (GRMSE, 2014)

Obstacles constrained Mars powered descent trajectory optimization via navigation function. - Haijing Hu; Shengying Zhu; Pingyuan Cui (ICIA, 2015)

A geometric dynamic temporal reasoning method with tags. - Rui Xu 027; Zhaoyu Li; Pingyuan Cui; Shengying Zhu; Ai Gao (ICCI*CC, 2016)

An Action Guided Constraint Satisfaction Technique for Planning Problem. - Xiao Jiang; Pingyuan Cui; Rui Xu 027; Ai Gao; Shengying Zhu (Int. J. Softw. Sci. Comput. Intell., 2016)

A Geometric Dynamic Temporal Reasoning Method with Tags for Cognitive Systems. - Rui Xu 027; Zhaoyu Li; Pingyuan Cui; Shengying Zhu; Ai Gao (Int. J. Softw. Sci. Comput. Intell., 2016)

A new algorithm for generation of dispatchable networks with temporal constraints. - Dexiang Chen; Rui Xu 027; Pingyuan Cui; Shengying Zhu; Zhaoyu Li (Enterp. Inf. Syst., 2017)

Geometry-based propagation of temporal constraints. - Zhaoyu Li; Rui Xu 027; Pingyuan Cui; Lida Xu; Wu He (Inf. Syst. Frontiers, 2017)

Trajectory curvature guidance for Mars landings in hazardous terrains. - Pingyuan Cui; Tong Qin; Shengying Zhu; Yang Liu; Rui Xu 027; Zhengshi Yu (Autom., 2018)

Observability-Based Navigation Using Optical and Radiometric Measurements for Asteroid Proximity. - He Jia; Shengying Zhu; Pingyuan Cui (IEEE Trans. Aerosp. Electron. Syst., 2020)

Collision Risk-Perceptive Landing Control for Small-Body Missions. - Dantong Ge; Pingyuan Cui (IEEE Trans. Aerosp. Electron. Syst., 2021)

Vector Trajectory Method for Obstacle Avoidance Constrained Planetary Landing Trajectory Optimization. - Jiateng Long; Pingyuan Cui; Shengying Zhu (IEEE Trans. Aerosp. Electron. Syst., 2022)

Closed-Loop Guidance for Asteroid Landing Using Stability-Related Control and Three-Dimensional Convex Curvature Constraints. - Pingyuan Cui; Chengyu Zhang 009; Zixuan Liang (IEEE Trans. Aerosp. Electron. Syst., 2023)

State Estimation With Nonlinear Inequality Constraints for Small Celestial Body Flexible Landing. - Pingyuan Cui; Zelong Chen; Dantong Ge; Shengying Zhu; Shisheng Cui (IEEE Trans. Aerosp. Electron. Syst., 2025)