A controller design method for drag-free spacecraft multiple loops with frequency domain constraints-Reference-Cited by-同舟云学术

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A controller design method for drag-free spacecraft multiple loops with frequency domain constraints

Published:2022 Issue: Volume: Page:1-14
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Ma Zhijie¹^ORCID,Wang Jihe²

Affiliation:

1. MOE Key Laboratory of TianQin Mission, TianQin Research Center for Gravitational Physics & School of Physics and Astronomy, Frontiers Science Center for TianQin, Gravitational Wave Research Center of CNSA, Sun Yat-sen University (Zhuhai Campus), Zhuhai, China

2. College of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China

Funder

Guangdong Major Project of Basic and Applied Basic Research

National Natural Science Foundation of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/7778228/09963627.pdf?arnumber=9963627

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear modeling and validation of spacecraft dynamics for space-based gravitational wave detector;Acta Astronautica;2024-11

2. Research on High-Stability Composite Control Methods for Telescope Pointing Systems under Multiple Disturbances;Sensors;2024-05-02

3. Payload architecture and pointing control strategies for TianQin;Physical Review D;2024-03-01

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