Robust H∞ dynamic output feedback control for spacecraft rendezvous with poles and input constraint
DOI10.1080/00207721.2016.1229082zbMath1362.93048OpenAlexW2523301333MaRDI QIDQ5347318
Publication date: 23 May 2017
Published in: International Journal of Systems Science (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/00207721.2016.1229082
\(H_\infty\) controllinear matrix inequalitiesinput constraintdynamic output feedback controlspacecraft rendezvous
Sensitivity (robustness) (93B35) Feedback control (93B52) (H^infty)-control (93B36) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)
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Cites Work
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