本发明涉及一种方法，用于从一个机载平台（4），其中，从所述机载平台（4）的导弹（2）下降滴下导弹（2）和利用至少一个可移动的控制表面（12）绕滚动运动 控制其纵轴。 为了防止导弹（2）与所述机载平台（4）放电的碰撞，所以建议舵（12）的机械阻挡元件的掉落之前（24）被阻挡，在放电过程中的舵（12） 通过闭锁元件的运动（24）是紧急释放的一部分，从而使舵（12）的导弹的预定飞行阶段（2）的舵后是可移动的仅在其方向舵偏转区域（44）和阻挡元件（24）的一部分（42） （12）完全解锁，以便其可在其整个方向舵偏转区域（44）上移动。

The invention relates to a method for dropping a guided missile (2) from an airborne platform (4), in which the missile (2) from the airborne platform (4) dropped and using at least one movable control surface (12) a rolling movement about controls its longitudinal axis. In order to prevent a collision of the guided missile (2) with the airborne platform (4) with discharge, it is proposed that the rudder (12) before dropping of a mechanical blocking element (24) is blocked, the rudder (12) during a discharge process by a movement of the blocking element (24) is part of emergency release, so that the rudder (12) is movable only over a part (42) of its rudder deflection region (44) and the blocking element (24) after a predetermined flight phase of the missile (2) the rudder (12) completely unlocked, so that it is movable over its entire rudder deflection region (44).