Attitude control for fly wing unmanned aerial vehicle with input constraints
ZHANG Bo
ZHU Xiao-ping
ZHOU Zhou
PENG Xin-chao
Keywords：unmanned aerial vehicles (UAV)nonlinear control systemsbacksteppinglinear matrix inequalities (LMIs)input constraintsextended state observer
Publication Date：2015-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：9( 725-733 )