Modeling and disturbance suppression for spacecraft solar array systems subject to drive fluctuation-Reference-Cited by-同舟云学术

Modeling and disturbance suppression for spacecraft solar array systems subject to drive fluctuation

Published:2021-01 Issue: Volume:108 Page:106398
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Jinlong,Lu Shaobo,Zhao Luyi

Funder

National Natural Science Foundation of China

Chongqing Research Program of Basic Research and Frontier Technology

Shanghai Aerospace S&T Innovation Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

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3. Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system;Chaka;Acta Astronaut.,2017

4. Adaptive fast nonsingular terminal sliding mode control for attitude tracking of flexible spacecraft with rotating appendage;Miao;Aerosp. Sci. Technol.,2019

5. Optimal robust position control with input shaping for flexible solar array drive system: a fuzzy-set theoretic approach;Xu;IEEE Trans. Fuzzy Syst.,2019

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