A method for the autonomous position control of guided missiles

摘要

a method for autonomous lagesteuerung of missiles, is that in a computer of the missile on the ground information on its current situation and flight and target dates will be entered.the computer input initial data by u00e4nderungswerte of the tru00e4gheitsnavigation and other navigationshilfsmitteln constantly being added to and implementation of the navigation weitergerechnet. the initial data by a vorstartgeru00e4t in the computer of the missile entered.the procedure allows the use of tru00e4gerflugzeugen, no data to the missile can produce.