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Optimal control of a tethered subsatellite of three degrees of freedom
D. P. Jin
*
,
H. Y. Hu
*
Corresponding author for this work
Nanjing University of Aeronautics and Astronautics
Research output
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Contribution to journal
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Article
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peer-review
48
Citations (Scopus)
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Engineering
Degree of Freedom
100%
Optimal Control
100%
Plane Motion
66%
Supports
33%
Quadratic Programming Problem
33%
State Variable
33%
Optimal Control Problem
33%
Mathematics
Programming Problem
33%
Vertical Axis
33%
State Variable
33%