| 摘要 |
<p>The system has a flow deflector (6) moving outside a nozzle (3), and penetrating into an output stream of the nozzle so as to cause deviation of a cylindrical mobile i.e. missile (1). A guiding unit angularly guides the deflector in rotation around a longitudinal axis (XX) of the mobile before launching the mobile so as to allow in-flight deviation of the mobile in a vertical plane passing through a launching point and a target point by an action of the deflector, where the mobile is initially launched by a launching tube of the guiding unit.</p> |
