Intelligent cooperative guidance method for spacecraft under multi-information incompleteness

<p indent="0mm">In multi-role game scenarios involving spacecraft, such as “target-pursuer-defender”, the primary challenge lies in the collaborative guidance game where the target and defender work together against the pursuer. Given the incomplete prior and observational information in such scenarios, including uncertainties in opponent guidance strategies, missing detection data, and measurement noise, this paper proposes an intelligent cooperative guidance method based on an adaptive dueling double deep Q-network (AD<sup>3</sup>QN). Firstly, to address the issue of sparse rewards during agent training, a continuous reward function is constructed using the environmental potential function, ensuring the optimality of the derived guidance strategy concerning the reward function. Secondly, leveraging the feature extraction capabilities of convolutional neural networks and the sequential data modeling capabilities of gated recurrent unit networks, a novel hybrid network architecture is developed to enhance the agent’s ability to estimate observational information and identify prior information. Furthermore, a mechanism for handling incomplete information is designed based on the spatiotemporal continuity of the spacecraft’s motion state and the operational characteristics of the network architecture. By expanding the set of incomplete information over the time dimension, this mechanism fully characterizes the real flight state and unknown strategy trajectory features, achieving efficient convergence of the decision network under various incomplete information conditions. Finally, numerical simulations validate the effectiveness of the proposed method, and comparative simulations demonstrate its superiority in spacecraft evasion performance.

Authors

Publication Details

Journal
Zhongguo kexue. Wulixue Lixue Tianwenxue
Published
2025-05-06
DOI
https://doi.org/10.1360/sspma-2024-0292
Primary Topic
Guidance and Control Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

Intelligent cooperative guidance method for spacecraft under multi-information incompleteness

J. Wang, Haizhao Liang, Weilin Ni, Peihuan Qiu
Zhongguo kexue. Wulixue Lixue Tianwenxue
Guidance and Control Systems
article

Intelligent cooperative guidance method for spacecraft under multi-information incompleteness

J. Wang, Haizhao Liang, Weilin Ni, Peihuan Qiu
article en

Abstract

<p indent="0mm">In multi-role game scenarios involving spacecraft, such as “target-pursuer-defender”, the primary challenge lies in the collaborative guidance game where the target and defender work together against the pursuer. Given the incomplete prior and observational information in such scenarios, including uncertainties in opponent guidance strategies, missing detection data, and measurement noise, this paper proposes an intelligent cooperative guidance method based on an adaptive dueling double deep Q-network (AD<sup>3</sup>QN). Firstly, to address the issue of sparse rewards during agent training, a continuous reward function is constructed using the environmental potential function, ensuring the optimality of the derived guidance strategy concerning the reward function. Secondly, leveraging the feature extraction capabilities of convolutional neural networks and the sequential data modeling capabilities of gated recurrent unit networks, a novel hybrid network architecture is developed to enhance the agent’s ability to estimate observational information and identify prior information. Furthermore, a mechanism for handling incomplete information is designed based on the spatiotemporal continuity of the spacecraft’s motion state and the operational characteristics of the network architecture. By expanding the set of incomplete information over the time dimension, this mechanism fully characterizes the real flight state and unknown strategy trajectory features, achieving efficient convergence of the decision network under various incomplete information conditions. Finally, numerical simulations validate the effectiveness of the proposed method, and comparative simulations demonstrate its superiority in spacecraft evasion performance.

Zhongguo kexue. Wulixue Lixue TianwenxueVol. 55(9)
Openalex Percentile: Top 87%
Guidance and Control Systems
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