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PDE Model-Based Boundary Control of a Spacecraft with Double Flexible Appendages under Prescribed Performance
Ma, Junteng, Wen, Hao, Jin, DongpingLanguage:
english
Journal:
Advances in Space Research
DOI:
10.1016/j.asr.2019.09.050
Date:
October, 2019
File:
PDF, 1.29 MB
english, 2019