Fault-tolerant reconfigurable control of tailless aircraft based on self-adaptive PID technology;
基于自适应PID技术的无尾飞机容错重构控制
A drag rudder is mostly used by tailless aircraft.
阻力方向舵在无尾飞机上得到广泛的应用。
The W-shaped tailless aircraft has not stabilizer and vertical tail,and it is based on the design of forward-swept wing and the integrated design of blended wing-fuselage.
W型无尾飞机基于前掠翼及翼身融合的一体化设计,取消了平尾和垂尾,可大幅降低雷达反射截面积,减轻结构重量;同时具有亚声速气动效率高、横航向操纵面效率高的优势。
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