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Di Wu

Orcid: 0000-0002-5214-962X

Affiliations:
  • Beihang University,School of Astronautics, State Key Laboratory of High-Efficiency Reusable Aerospace Transportation Technology, Beijing, China
  • Tsinghua University, School of Aerospace Engineering, Beijing, China


According to our database1, Di Wu authored at least 11 papers between 2020 and 2026.

Collaborative distances:
  • Dijkstra number2 of five.
  • Erdős number3 of five.

Timeline

Legend:

Book  In proceedings  Article  PhD thesis  Dataset  Other 

Links

Online presence:

On csauthors.net:

Bibliography

2026
Compliance- and Reliability-Based Bidesign for Space Manipulator Controller With Correlated Uncertainties and Actuator Degradation.
[BibTeX]
[DOI]
Chen Yang
,
Yulan Liao
,
Shengping Gong
,
Peng Shi
,
Lin Cheng
,
Di Wu
IEEE Trans. Aerosp. Electron. Syst., 2026

Gauss-Legendre Accelerated Double-Iteration Method for Asteroid Landing Trajectory Planning.
[BibTeX]
[DOI]
Xiaotong Wu
,
Zibin Sun
,
Di Wu
,
Lin Cheng
,
Shengping Gong
IEEE Trans. Aerosp. Electron. Syst., 2026

Deep Neural Network-Based High-Precision Identification of Weak Stability Boundary Structures.
[BibTeX]
[DOI]
Shuyue Fu
,
Ziqi Xu
,
Di Wu
,
Shengping Gong
IEEE Trans. Aerosp. Electron. Syst., 2026

Robust Model-Based Reinforcement Learning for Rocket Landing.
[BibTeX]
[DOI]
Donghe Chen
,
Di Wu
,
Lin Cheng
,
Shengping Gong
IEEE Trans. Aerosp. Electron. Syst., 2026

2025
Recursive Inference for Heterogeneous Multi-Output GP State-Space Models with Arbitrary Moment Matching.
[BibTeX]
[DOI]
Tengjie Zheng
,
Jilan Mei
,
Di Wu
,
Lin Cheng
,
Shengping Gong
CoRR, October, 2025

Learning-Based Stable Optimal Control for Infinite-Time Nonlinear Regulation Problems.
[BibTeX]
[DOI]
Han Wang
,
Di Wu
,
Lin Cheng
,
Shengping Gong
,
Xu Huang
CoRR, June, 2025

Solution Space of Minimum-Time Low-Thrust Rephasing in Elliptical Orbit.
[BibTeX]
[DOI]
Di Wu
,
Lin Cheng
,
Shengping Gong
,
Hexi Baoyin
IEEE Trans. Aerosp. Electron. Syst., February, 2025

2024
Fuel-Optimal Control for Multiple Spacecraft Formation Flying With Relative Motion Constraints.
[BibTeX]
[DOI]
Wei Wang
,
Di Wu
,
Hexi Baoyin
IEEE Trans. Aerosp. Electron. Syst., December, 2024

Multiphase Homotopic Approaches for Best Solution to Low-Thrust Geocentric Trajectories.
[BibTeX]
[DOI]
Xiang Guo
,
Di Wu
,
Fanghua Jiang
IEEE Trans. Aerosp. Electron. Syst., August, 2024

2022
Optimal Projected Circular Orbit for Spacecraft Formation Flying Near a Slowly Rotating Asteroid.
[BibTeX]
[DOI]
Wei Wang
,
Di Wu
,
Ran Sun
,
Hexi Baoyin
IEEE Trans. Aerosp. Electron. Syst., 2022

2020
Warm-Start Multihomotopic Optimization for Low-Thrust Many-Revolution Trajectories.
[BibTeX]
[DOI]
Di Wu
,
Lin Cheng
,
Junfeng Li
IEEE Trans. Aerosp. Electron. Syst., 2020


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