Underactuated Attitude–Orbit Coupling Control for Microsatellite Based on a Single Orbital Thruster-Reference-Cited by-同舟云学术

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Underactuated Attitude–Orbit Coupling Control for Microsatellite Based on a Single Orbital Thruster

Published:2024-04 Issue:2 Volume:60 Page:2082-2092
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Lu Junjie¹^ORCID,Meng Zhongjie¹^ORCID

Affiliation:

1. Northwestern Polytechnical University, Xi'an, China

Funder

National Natural Science Foundation of China

Natural Science Basic Research Plan in Shaanxi Province of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/7/10496926/10388276.pdf?arnumber=10388276

Reference34 articles.

1. Optimization of satellite constellation deployment strategy considering uncertain areas of interest

2. Dynamic Simulation of Space Debris Cloud Capture Using the Tethered Net

3. Small satellites an overview and assessment

4. Prospects for the Future Development of China’s Space Transportation System

5. An Overview of Cube-Satellite Propulsion Technologies and Trends

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