Shengying Zhu

Orcid: 0000-0003-1414-4948

According to our database¹, Shengying Zhu authored at least 21 papers between 2013 and 2025.

Collaborative distances:

Dijkstra number² of five.
Erdős number³ of five.

Timeline

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PhD thesis

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On csauthors.net:

Bibliography

2025

Input-Saturated Station Keeping for Celestial Body Orbits Using Iterative Learning Control.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., June, 2025

Powered Descent Guidance Using a Tunable Segmented Acceleration Profile.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., April, 2025

State Estimation With Nonlinear Inequality Constraints for Small Celestial Body Flexible Landing.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., April, 2025

Asteroid Approach Guidance Based on Predicted Rendezvous Probability.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., February, 2025

Distributed incremental arc-consistency reasoning method for temporal network in multi-probe collaborative mission planning.

[BibT_eX]

[DOI]

Knowl. Based Syst., 2025

2024

Deep reinforcement learning based planning method in state space for lunar rovers.

[BibT_eX]

[DOI]

Eng. Appl. Artif. Intell., January, 2024

2023

Lateral Entry Guidance With Terminal Time Constraint.

[BibT_eX]

[DOI]

Zixuan Liang

Chang Lv

Shengying Zhu

IEEE Trans. Aerosp. Electron. Syst., June, 2023

Hierarchical multi-agent planning for flexible assembly of large-scale lunar facilities.

[BibT_eX]

[DOI]

Adv. Eng. Informatics, January, 2023

2022

Vector Trajectory Method for Obstacle Avoidance Constrained Planetary Landing Trajectory Optimization.

[BibT_eX]

[DOI]

Jiateng Long

Pingyuan Cui

Shengying Zhu

IEEE Trans. Aerosp. Electron. Syst., 2022

2021

Rapid Generation of the Fuel-Optimal Trajectory for Landing on Irregularly Shaped Asteroids.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., 2021

2020

Extended State-Based Planning Approach for Deep Space Exploration.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., 2020

Observability-Based Navigation Using Optical and Radiometric Measurements for Asteroid Proximity.

[BibT_eX]

[DOI]

He Jia

Shengying Zhu

Pingyuan Cui

IEEE Trans. Aerosp. Electron. Syst., 2020

2018

Trajectory curvature guidance for Mars landings in hazardous terrains.

[BibT_eX]

[DOI]

Autom., 2018

2017

A rapid maneuver path planning method with complex sensor pointing constraints in the attitude space.

[BibT_eX]

[DOI]

Inf. Syst. Frontiers, 2017

A new algorithm for generation of dispatchable networks with temporal constraints.

[BibT_eX]

[DOI]

Enterp. Inf. Syst., 2017

2016

A Geometric Dynamic Temporal Reasoning Method with Tags for Cognitive Systems.

[BibT_eX]

[DOI]

Int. J. Softw. Sci. Comput. Intell., 2016

An Action Guided Constraint Satisfaction Technique for Planning Problem.

[BibT_eX]

[DOI]

Int. J. Softw. Sci. Comput. Intell., 2016

A geometric dynamic temporal reasoning method with tags.

[BibT_eX]

[DOI]

Proceedings of the 15th IEEE International Conference on Cognitive Informatics & Cognitive Computing , 2016

2015

Obstacles constrained Mars powered descent trajectory optimization via navigation function.

[BibT_eX]

[DOI]

Haijing Hu

Shengying Zhu

Pingyuan Cui

Proceedings of the IEEE International Conference on Information and Automation, 2015

2013

Fast matching of feature point and relative motion estimation for asteroid landing phase.

[BibT_eX]

[DOI]

Proceedings of the 10th IEEE International Conference on Control and Automation, 2013

Maneuver sequence planning for autonomous navigation based on multiple asteroid images.

[BibT_eX]

[DOI]

Proceedings of the 10th IEEE International Conference on Control and Automation, 2013

Shengying Zhu

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