Fully-actuated-system-approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying
Author:
Affiliation:
1. Harbin Institute of Technology,Research Center of Satellite Technology,Harbin,150001
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10243163/10243123/10243360.pdf?arnumber=10243360
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1. Formation control of under-actuated multi-robot vehicle systems based on high-order fully actuated systems approach;2024 3rd Conference on Fully Actuated System Theory and Applications (FASTA);2024-05-10
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