METHOD OF RELIABILITY IMPROVEMENT OF AIR-TO-SURFACE MISSILES CONTROL EQUIPMENT
The article analyzes the current state of the fleet of guided air means of destruction (missiles), the problems of repair and extension of the resource. The article substantiates the need for the transition of guided air missile of the "air-to-surface" class to operation according to the technical condition. The shortcomings of the existing inspection system for the technical condition of guided air weapon are shown. For the existing inspection system of technical operation of guided air weapon, one of the areas that will solve the problem of maintaining the combat readiness of aircraft is the transition to the operation of guided air weapon in technical condition. It is shown that the transition of guided air missiles to operation according to the technical condition and modernization of unguided air missiles involves strengthening the role of operations to measure and control their parameters and characteristics in order to determine the actual technical condition and make informed decisions about their further operation. Peculiarities of appearance of the Type 1 and Type 2 errors during control of a technical condition of aviation armament are presented. A method of increasing the reliability of air-to-surface missile control equipment by conducting control checks in the inter-check interval is proposed. The fundamental difference between the proposed information-redundant model of operation of guided air missiles and the classic model is the introduction into the system of operation a new diagnostic operation - an intermediate control check. Peculiarities of application of the developed method concerning calculation of both quantity of control checks and their periodicity within an inter-check interval are shown.