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Disturbance-Free Payload spacecraft modeling and control:Non-contact architecture for high-precision space missions

Wei Zhang Yanbin Zhao Dongyu Li

航天动力学（英文）2026，Vol.10Issue(1)：1-24,24.

航天动力学（英文）2026，Vol.10Issue(1)：1-24,24.DOI:10.1007/s42064-025-0266-4

Disturbance-Free Payload spacecraft modeling and control:Non-contact architecture for high-precision space missions

Wei Zhang ¹Yanbin Zhao ¹Dongyu Li¹

作者信息

1. Shanghai Institute of Satellite Engineering,Shanghai 201109,China||Shanghai Key Laboratory of Deep Space Exploration Technology,Shanghai 201109,China
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摘要

关键词

Disturbance-Free Payload(DFP)spacecraft/non-contact actuator/dynamic modeling/relative levitation state/position and attitude control

Key words

Disturbance-Free Payload(DFP)spacecraft/non-contact actuator/dynamic modeling/relative levitation state/position and attitude control

引用本文复制引用

Wei Zhang,Yanbin Zhao,Dongyu Li..Disturbance-Free Payload spacecraft modeling and control:Non-contact architecture for high-precision space missions[J].航天动力学（英文）,2026,10(1):1-24,24.

基金项目

This work was supported by the National Natural Science Foundation of China under Grants U24B20157 and 62473023,the Fundamental Research Funds for the Central Universities,the National Natural Science Foundation of China under Grant 62303132,and the Beijing Natural Science Foundation under Grant 4242043. （）

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