摘要
Y2002-63520-217 0324502通过2级线性化的非线性非最小相位 VTOL 宇宙飞船的飞行控制设计=Flight control design for a nonlin-ear non-minimum phase VTOL aircraft via two-step lin-earizalion[会,英]/Saeki,M.& Sakaue,Y.//Proceed-ings of the 40th IEEE Conference on Decision and Con-trol,Vol.1 of 5,—217～222(HE)
出处
《电子科技文摘》
2003年第10期167-171,共5页
Sci.& Tech.Abstract
