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<p>pitch control. They do so by decreasing or increasing the downward force created by the stabilizer:<br/>
* an increased downward force, produced by up elevator, forces the tail down and the nose up. At constant speed, the wing's increased angle of attack causes a greater <a href="page.php?w=lift_%28force%29">lift</a> to be produced by the wing, accelerating the aircraft upwards. The drag and power demand also increase;<br/>
* a decreased downward force at the tail, produced by down elevator, causes the tail to rise and the nose to lower. At constant</p><p>
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