New Minimum InfnityNorm Solution and Rapid Eigenaxis Attitude Maneuvering of Spacecraft

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Publisher
SPRINGER HEIDELBERG
Issue Date
2022-12
Language
English
Article Type
Correction
Citation

JOURNAL OF THE ASTRONAUTICAL SCIENCES, v.69, no.6, pp.988 - 1016

ISSN
0021-9142
DOI
10.1007/s40295-022-00355-7
URI
http://hdl.handle.net/10203/304174
Appears in Collection
AE-Journal Papers(저널논문)
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