An Analytical Impulse Thrust Strategy in Spacecraft Pursuit-Evasion Games with Mass Variation and Perception Frequency

The domain of astrodynamics is witnessing a surge in scholarly interest, particularly concerning the spacecraft pursuit-evasion games. This treatise introduces an analytical methodology designed to deduce the optimal impulsive thrust game-theoretic strategies for spacecraft, considering both mass variation and the sensory limitations inherent in systems. The methodology commences by computationally delineating the relative reachable domain difference from a spatial geometry standpoint. Then, each spacecraft computes a threat index predicated on its perceptive faculties and the prevailing engagement geometry, then it strategically deploys thrust to precipitously diminish this index. The efficacy of the proposed analytical technique is corroborated by the simulation experiment. Given the analytical nature of the computations entailed, the approach holds significant promise for on-board application.

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Publication Details

Published
2024-11-01
DOI
https://doi.org/10.1109/cac63892.2024.10865324
Citations
1
Primary Topic
Guidance and Control Systems
Type
article
Field-Weighted Citation Impact
1.30
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article

An Analytical Impulse Thrust Strategy in Spacecraft Pursuit-Evasion Games with Mass Variation and Perception Frequency

Leping Yang, Chengming Zhang, Yanwei Zhu
1 citations
Guidance and Control Systems
1.30
article

An Analytical Impulse Thrust Strategy in Spacecraft Pursuit-Evasion Games with Mass Variation and Perception Frequency

Leping Yang, Chengming Zhang, Yanwei Zhu
article en
1 citations

Abstract

The domain of astrodynamics is witnessing a surge in scholarly interest, particularly concerning the spacecraft pursuit-evasion games. This treatise introduces an analytical methodology designed to deduce the optimal impulsive thrust game-theoretic strategies for spacecraft, considering both mass variation and the sensory limitations inherent in systems. The methodology commences by computationally delineating the relative reachable domain difference from a spatial geometry standpoint. Then, each spacecraft computes a threat index predicated on its perceptive faculties and the prevailing engagement geometry, then it strategically deploys thrust to precipitously diminish this index. The efficacy of the proposed analytical technique is corroborated by the simulation experiment. Given the analytical nature of the computations entailed, the approach holds significant promise for on-board application.

National University of Defense Technology (CN)
Openalex Percentile: Top 11%
Guidance and Control Systems
1.30
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An Analytical Impulse Thrust Strategy in Spacecraft Pursuit-Evasion Games with Mass Variation and Perception Frequency — Leping Yang, Chengming Zhang, et al. · (2024) | TGRS Research Map | TGRS