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Published in 2019 at "IEEE Access"
DOI: 10.1109/access.2019.2905371
Abstract: In this paper, an improved extended state observer (ESO) based on sigmoid function and a finite-time convergence attitude controller are designed for reusable launch vehicle (RLV) in the re-entry phase. First, a control-oriented model (COM)…
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Keywords:
rlv entry;
finite time;
entry phase;
rlv ... See more keywords