Proportional fuzzy feed-forward architecture control validation by wind tunnel tests of a morphing wing
control system、flexible skin、aerodynamic optimization、performance improvement、aerodynamic performance、composite materials、experimental model、wind tunnel tests、transition point、wing structure、real time、in order
30
TP2;V21
2017-05-19(万方平台首次上网日期,不代表论文的发表时间)
共16页
561-576