Asymmetric Deep Reinforcement Learning-Based Spacecraft Approaching Maneuver Under Unknown Disturbance

Spacecraft approaching maneuver control normally uses traditional control methods such as Proportional–Integral–Derivative (PID) or Model Predictive Control (MPC), which require meticulous system design and lack robustness against unknown disturbances. To address these limitations, we propose an end-to-end asymmetric Deep Reinforcement Learning-based (DRL) spacecraft approaching maneuver (ADSAM) algorithm, which significantly enhances the robutsness of the space-approaching maneuver under large-scale unknown disturbance and Partial Observation Markov Decision Processes (POMDPs). We present a numerical simulation environment with the linear Clohessy–Wiltshire (CW) model, incorporating the Runge–Kutta 4th order method (RK4) to ensure a more accurate and efficient state transition. Experimental results also demonstrate that the effectiveness of the proposed algorithm outperforms the-state-of-the-art methods.

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Publication Details

Journal
Aerospace
Published
2025-02-20
DOI
https://doi.org/10.3390/aerospace12030170
Citations
2
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
9.99

Funders

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article

Asymmetric Deep Reinforcement Learning-Based Spacecraft Approaching Maneuver Under Unknown Disturbance

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article

Asymmetric Deep Reinforcement Learning-Based Spacecraft Approaching Maneuver Under Unknown Disturbance

Dong Zhou, Runran Deng, Shibo Shao, Weizhao Ma, Guanghui Sun
article en
2 citations

Abstract

Spacecraft approaching maneuver control normally uses traditional control methods such as Proportional–Integral–Derivative (PID) or Model Predictive Control (MPC), which require meticulous system design and lack robustness against unknown disturbances. To address these limitations, we propose an end-to-end asymmetric Deep Reinforcement Learning-based (DRL) spacecraft approaching maneuver (ADSAM) algorithm, which significantly enhances the robutsness of the space-approaching maneuver under large-scale unknown disturbance and Partial Observation Markov Decision Processes (POMDPs). We present a numerical simulation environment with the linear Clohessy–Wiltshire (CW) model, incorporating the Runge–Kutta 4th order method (RK4) to ensure a more accurate and efficient state transition. Experimental results also demonstrate that the effectiveness of the proposed algorithm outperforms the-state-of-the-art methods.

AerospaceVol. 12(3)
Chinese University of Hong Kong (HK), China Academy of Space Technology (CN), Harbin Institute of Technology (CN)
National Natural Science Foundation of China
Openalex Percentile: Top 3%
Space Satellite Systems and Control
9.99
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