Shengping Gong

Orcid: 0000-0002-1910-2918

According to our database1, Shengping Gong authored at least 18 papers between 2015 and 2025.

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

Timeline

Legend:

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Links

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Bibliography

2025
Autonomous Vision-Based Control for Spacecraft Navigation Around an Asteroid.
IEEE Trans. Aerosp. Electron. Syst., August, 2025

Ascent Trajectory Optimization for Boost-Glide Vehicle Using Homotopy Approximation Function Sequential Convex Programming.
IEEE Trans. Aerosp. Electron. Syst., June, 2025

Robust Incremental Learning of Approximate Dynamic Programming for Nonlinear Optimal Guidance.
IEEE Trans. Aerosp. Electron. Syst., June, 2025

Learning-Based Stable Optimal Control for Infinite-Time Nonlinear Regulation Problems.
CoRR, June, 2025

Convex Formulation and Efficiency Enhancement for Powered Landing Guidance With Second-Order Cone Probability Constraints.
IEEE Trans. Aerosp. Electron. Syst., April, 2025

Stability Enhancement in Reinforcement Learning via Adaptive Control Lyapunov Function.
CoRR, April, 2025

Confidence-Aware Learning Optimal Terminal Guidance via Gaussian Process Regression.
CoRR, April, 2025

Solution Space of Minimum-Time Low-Thrust Rephasing in Elliptical Orbit.
IEEE Trans. Aerosp. Electron. Syst., February, 2025

Spacecraft angular velocity estimation from inertial vector measurements: A parameter estimation approach.
Autom., 2025

2024
Neural-Network-Based Nonlinear Optimal Terminal Guidance With Impact Angle Constraints.
IEEE Trans. Aerosp. Electron. Syst., February, 2024

Recursive Gaussian Process State Space Model.
CoRR, 2024

Parameter Estimation Based Angular Velocity Observer Design for Rigid-Body Spacecraft.
Proceedings of the European Control Conference, 2024

2022
Successive Convexification for Ascent Trajectory Replanning of a Multistage Launch Vehicle Experiencing Nonfatal Dynamic Faults.
IEEE Trans. Aerosp. Electron. Syst., 2022

2020
Pursuit-Evasion Game for Satellites Based on Continuous Thrust Reachable Domain.
IEEE Trans. Aerosp. Electron. Syst., 2020

2019
Solar-Sail Trajectory Design of Multiple Near Earth Asteroids Exploration Based on Deep Neural Network.
CoRR, 2019

Solar-Sail Deep Space Trajectory Optimization Using Successive Convex Programming.
CoRR, 2019

2015
A new inclination cranking method for a flexible spinning solar sail.
IEEE Trans. Aerosp. Electron. Syst., 2015

Optimal attitude maneuver of an axisymmetric spinning solar sail.
IEEE Trans. Aerosp. Electron. Syst., 2015


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