Conducted research aimed at substantiation of the rational system of measuring, collecting and processing information in accordance with the requirements of ensuring flight tests of rocket-space equipment and missile armament, in which the complex of devices is regarded as information-measuring technical system.
Common elements identified that make up the content of its functioning, which are a set of coordinated information processes performed by technical devices and determine the structural and functional decomposition of the system. The modular construction of the methodology for substantiating the alternative of forming a complex of devices of measuring, collection and processing has been substantiated, which ensures sufficient autonomy for conducting studies to substantiate subsystem variants, as well as the necessary interconnection (in terms of input and output parameters) when combined into successive research schemes. The proposed methodology consists of three interconnected private methods:
- method of rational measurement subsystem configuration justification;
- method of rational justification configure the subsystem the processing and analysis of measurement information;
- method of rational justification of the configuration of the subsystem information exchange.
Private methods designed to search the optimal values of variable parameters of the subsystems of a complex of devices of measurements, collection and treatment and aims to ensure the criteria of quality indicators that best meet the objectives of the relevant sub-systems and the needs of information support of flight tests of rocket and space technology and missile armament.
On the basis of the developed methodology, applied studies have been conducted to determine the rational version of the complex of tools for specific conditions and initial data of information support for the launch and flight of rocket-space technics and missile armament and evaluation of their results. Applied research on the basis of real launch data showed the advantages of the proposed approach to the formation of a set of tools compared to the existing one, while providing an indissoluble reception of the entire volume of information from the board of the product and the continuous delivery of the information required for flight control of the product with lower costs of the resources of the devices of receiving and transmitting information.