通过风洞试验，对带升降副翼控制的自由翼气动特性也进行了实验研究，验证了位于自由翼后缘的升降副翼可有效地控制自由翼相对气流的平衡迎角。
The aerodynamic characteristics of the free wing are investigated in this paper. The wind tunnel test results shows that the control of the angle of attack of the fre…
控制舵面：副翼，升降，方向。
随动补偿片，铰接在操纵面后缘(副翼，方向舵，升降舵)的可动部。
BALANCE TAB, a small hinged moveable part on the trailing edge of a control surface (aileron, elevator, rudder).
辅助操纵系统由升降舵调整片、副翼调整片、副翼随动补偿调整片和方向舵补偿调整片组成。
Assisted by the elevator control system to adjust on-chip, chip aileron adjustment, moving with the aileron and rudder-chip compensation adjustment compensation adjustment film composition.
针对此翼面上有升降舵的多舵面布局，建立了俯仰运动下不同于翼面上只有副翼的动力学模型。
About multi - control surface configuration with elevators, its dynamic model was established under pitch movement, differing from wing with ailerons alone.
对于前轮转弯系统，脚踏板传感器组件通过升降舵副翼计算机向刹车和转弯控制组件发送信号。
The pedal transducer units send data to the BSCU via the ELACs for the nosewheel steering system.
对于前轮转弯系统，脚踏板传感器组件通过升降舵副翼计算机向刹车和转弯控制组件发送信号。
The pedal transducer units send data to the BSCU via the ELACs for the nosewheel steering system.
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