| 摘要 |
<p>The present invention pertains to the field of arms and ammunitions and essentially relates to methods for controlling aircraft having a descending phase during the passive flight trajectory in the atmosphere and comprising an inertial system, an onboard calculator as well as an active radio-localisation or passive optical seeker head. According to this method, the flight of the aerodynamic aircraft takes place according to an arbitrary trajectory during the descending flight phase until a predetermined turn area is reached. The method further involves redirecting the velocity vector of the aircraft and switching into a gliding flight mode. During the trajectory descending phase, the velocity vector of the aircraft is reoriented step by step in a vertical plane and towards the top.</p> |
