LMI-based Robust Auto-landing Controller Design Using Mixed H2/H infinity for Fixed wing UAV

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Publisher
한국자동제어학술회의
Issue Date
2009-09
Language
KOR
Citation

한국자동제어학술회의(KACC) 2009

URI
http://hdl.handle.net/10203/176430
Appears in Collection
EE-Conference Papers(학술회의논문)
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