Shuang Li

Orcid: 0000-0001-9142-5036

Affiliations:
  • Nanjing University of Aeronautics and Astronautics, College of Astronautics, China
  • Harbin Institute of Technology, School of Astronautics, Deep Space Exploration Research Center, China (former)


According to our database1, Shuang Li authored at least 18 papers between 2008 and 2024.

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

Timeline

Legend:

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PhD thesis 
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Links

Online presence:

On csauthors.net:

Bibliography

2024
An Automatic Control Perspective on Parameterizing Generative Adversarial Network.
IEEE Trans. Cybern., March, 2024

Real-Time Satellite Constellation Scheduling for Event-Triggered Cooperative Tracking of Space Objects.
IEEE Trans. Aerosp. Electron. Syst., 2024

2023
Combined Fuzzy Sliding-Mode Attitude Stabilization and Energy Storage for Small Satellite.
IEEE Trans. Aerosp. Electron. Syst., December, 2023

The SSR Brightness Temperature Increment Model Based on a Deep Neural Network.
Remote. Sens., September, 2023

Pseudospectral Convex Optimization Based Model Predictive Static Programming for Constrained Guidance.
IEEE Trans. Aerosp. Electron. Syst., June, 2023

Activities to Promote the Moon as an Absolute Calibration Reference.
Remote. Sens., May, 2023

Geolocation of Lunar Observations With JiLin-1 High-Resolution Optical Sensor.
IEEE Trans. Geosci. Remote. Sens., 2023

2022
Taming mode collapse in generative adversarial networks using cooperative realness discriminators.
IET Image Process., 2022

Mars Entry Trajectory Planning with Range Discretization and Successive Convexification.
CoRR, 2022

2021
Quantum-Interference Artificial Neural Network With Application to Space Manipulator Control.
IEEE Trans. Aerosp. Electron. Syst., 2021

Collision-Free Trajectory Design for Long-Distance Hopping Transfer on Asteroid Surface Using Convex Optimization.
IEEE Trans. Aerosp. Electron. Syst., 2021

Integration of gradient guidance and edge enhancement into super-resolution for small object detection in aerial images.
IET Image Process., 2021

2020
Fuel-Optimal Asteroid Descent Trajectory Planning Using a Lambert Solution-Based Costate Initialization.
IEEE Trans. Aerosp. Electron. Syst., 2020

Adaptive mesh refinement method for solving optimal control problems using interpolation error analysis and improved data compression.
J. Frankl. Inst., 2020

Robust coordinated control for large flexible spacecraft based on consensus theory.
J. Frankl. Inst., 2020

2019
Close-Range Angles-Only Relative Navigation of Multi-agent Cluster for On-Orbit Servicing Mission.
Proceedings of the Intelligent Robotics and Applications - 12th International Conference, 2019

2012
Robust sliding mode guidance and control for soft landing on small bodies.
J. Frankl. Inst., 2012

2008
Computer Vision Based Autonomous Navigation for Pin-Point Landing Robotic Spacecraft on Asteroids.
Proceedings of the Intelligent Robotics and Applications, First International Conference, 2008


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