Investigation of longitudinal aerodynamic parameters identification method for fly-by-wire passenger airliners
identification method、aerodynamic parameters、parameters identification、flight control system、energy distribution、frequency response、parameter design、Flight Simulator、method of、mode of
TJ7;TP2
2013-11-20(万方平台首次上网日期,不代表论文的发表时间)
共10页
1156-1165