Combined Fuzzy Sliding-Mode Attitude Stabilization and Energy Storage for Small Satellite-Reference-Cited by-同舟云学术

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Combined Fuzzy Sliding-Mode Attitude Stabilization and Energy Storage for Small Satellite

Published:2023-12 Issue:6 Volume:59 Page:7725-7738
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Wang Beichao¹^ORCID,Li Shuang¹^ORCID,Zhang Qingjun²^ORCID,Xin Ming³^ORCID

Affiliation:

1. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing, China

2. Institute of Remote Sensing Satellite, China Academy of Space Technology, Beijing, China

3. Department of Mechanical and Aerospace Engineering, University of Missouri, Columbia, MO, USA

Funder

National Natural Science Foundation of China

Qinglan Project of Jiangsu Province of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/10353051/10184469.pdf?arnumber=10184469

Reference37 articles.

1. Smaller Satellites, Larger Constellations: Trends and Design Issues for Earth Observation Systems

2. Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)

3. Development and Experimentation of a CubeSat Magnetic Attitude Control System Testbed

4. A combined energy and attitude control system for small satellites

5. Onboard errors of the combined energy and attitude control system

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