决定特定的标的手段舵---副翼（Rudder-Aileron）联动，标的手段舵-升降舵（Rudder-Elevator）联动，将标的手段舵向一侧打满，尔后插手升降舵向上（或向下）5％的联动尔后从头试飞，视察必要的升降舵量能否修改，每次测试都在...
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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).
由机头朝向操控者的倒飞停悬，将升降舵打降舵使直升机翻滚为机尾朝向操控者的正立停悬姿态，保持静止停悬5秒钟。
From this inverted Nose-In hover, add forward cyclic and flip the helicopter back to an upright Tail-In hover, hold for five (5) seconds.
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.
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