METHOD FOR IMPLEMENTATION OF INTEGRATION OF AIMING-NAVIGATION COMPLEX ON HELICOPTER OF TYPE MI-24

摘要

At implementation of method of integration of aiming-navigation complex on helicopter of type MI-24 one uses digital aiming-computing complex and multi-channel survey-aiming system. Cabin of helicopter is fitted with oculars for night vision. Control of position of axles of directional diagrams of channels of survey-aiming system is carried out by means of multi-functional control panel of operator’s control. Aiming and locking of target are performed through respective change by pilot of spatial position of helicopter and bringing into coincidence position of marker on multi-functional indicators with mark of target chosen. Finding out and identification of target by pilot y means of aiming-computer set determine aiming data according to parameters of flight of helicopter and chosen type of ammunition. One forms sight mark on reflector of viewfinder head of aiming-computer complex. Adaptation of devices is carried out through disconnection of electric circuits of built-in highlighting. Highlighting of all the devices is provided by means of external constructions with luminodiodes of respective color. Luminodiodes in external constructions are oriented in planes parallel to scales of the devices.