Method for decoupling unmanned, aerodynamic instable missile i.e. cruise missile, from carrier aircraft, involves automatically controlling missile by flight control mechanism and control device on basis of data stored in storage

摘要

The method involves separating electrical and mechanical between a missile (2) and a carrier aircraft (1). A flight control mechanism (32) of the missile is activated and the missile is automatically controlled by the control mechanism and control devices (23, 24) of the missile on basis of stabilization of flight condition changes, which are caused by downwind field prevailing between the missile and a carrier aircraft. The missile is automatically controlled by the mechanism and the control device on basis of data stored in a storage (34).