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Retrieval control of an electro-dynamic tethered satellite in an inclined orbit
Hao Wen
*
, Dongping Jin,
Haiyan Hu
*
Corresponding author for this work
Nanjing University of Aeronautics and Astronautics
Research output
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Article
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peer-review
8
Citations (Scopus)
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Engineering
Optimal Control
100%
Computer Simulation
50%
Control Scheme
50%
Control Action
50%
Optimal Trajectory
50%
Final Position
50%
Earth and Planetary Sciences
Tethered Satellite
100%
Electrodynamics
100%
Optimal Control
66%
Nonlinear Programming
33%
Physics
Optimal Control
100%
Electrodynamics
100%