A rapid decomposition method for remote sensing satellite missions based on the star-ground matching model

Autonomous task decomposition research in space is crucial. This paper proposes an approximate and analytical method for calculating time windows for point and small regional targets. It leverages satellite orbit patterns to establish models for sun-synchronous retrograde orbit distribution and satelliteground mapping, enabling rapid acquisition of time windows for point targets. Additionally, a boundary solving method based on slope-adaptive fitting is introduced for swiftly obtaining observation strips for regional targets. Simulation results show high precision and efficiency, with spatial-temporal errors at $\mathbf{0. 1 \%}$ and processing speeds in seconds, a significant improvement over traditional methods. This approach meets existing satellite platform requirements.

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Publication Details

Published
2024-09-22
DOI
https://doi.org/10.1109/apcap62011.2024.10881127
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
0.00

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article

A rapid decomposition method for remote sensing satellite missions based on the star-ground matching model

A. Li, Dexin Zhang, Wan Liu, Shichen Miao
Inertial Sensor and Navigation
article

A rapid decomposition method for remote sensing satellite missions based on the star-ground matching model

A. Li, Dexin Zhang, Wan Liu, Shichen Miao
article en

Abstract

Autonomous task decomposition research in space is crucial. This paper proposes an approximate and analytical method for calculating time windows for point and small regional targets. It leverages satellite orbit patterns to establish models for sun-synchronous retrograde orbit distribution and satelliteground mapping, enabling rapid acquisition of time windows for point targets. Additionally, a boundary solving method based on slope-adaptive fitting is introduced for swiftly obtaining observation strips for regional targets. Simulation results show high precision and efficiency, with spatial-temporal errors at $\mathbf{0. 1 \%}$ and processing speeds in seconds, a significant improvement over traditional methods. This approach meets existing satellite platform requirements.

Shanghai Jiao Tong University (CN), Shanghai Micro Satellite Engineering Center (CN)
Shanghai Academy of Spaceflight Technology
Climate action
Openalex Percentile: Top 54%
Inertial Sensor and Navigation
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