Method for engaging airborne targets using an air-to-air missile

摘要

The invention relates to a method for engaging airborne targets using an air-to-air missile, in which case, in order to increase the range, the missile is brought, in a first flight phase, onto a flight path (trajectory) which is directed upwards inclined at a predetermined angle, and this flight path is maintained until a predetermined time period has elapsed, before it is then guided to follow the target using the proportional navigation steering law. <IMAGE>