METHOD OF SPATIAL-TEMPORAL SYNTHESIS OF THE CONTROL LOOP MODEL OF UNMANNED FLYING VEHICLES INTO A DATA-CENTRIC ADS
- Authors
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- Keywords:
- control circuit, firing method, complex guidance model, air defense systems, architecture, unmanned aerial vehicle
- Abstract
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The article raises issues of development of the theory of data-oriented operations based on the methodology of the architectural approach in the creation of anti-aircraft missile systems. A method and model of synthesis of the model of unmanned aerial vehicle (UAV) control loop in the context of creating air defence missile systems (ADMS), unmanned weapons in an information-oriented automated control system, which is carried out during its operation in real time, are proposed.
The synthesis involves the selection of a firing method, tracking of operational states and processes during the formation of the SAM firing cycle, spatial and temporal decomposition of SAMs to determine the organisational and technical system of SAMs as part of an air defence missile system and the formation of a 4D control loop structure. For the defined 4D structure of the control loop, classes describing the main systems of the WME samples are formed, and functional models for the component parts (elements) of the WME are developed. A variant of docking models of individual samples of weapons and military equipment within the framework of synthesis of a complex model of the control scheme is proposed.
The article presents a general structural diagram of the method of spatio-temporal synthesis of the model of the control loop of an information-oriented automated control system, according to which the following are proposed 4D guidance loop structure synthesis scheme; system decomposition operation scheme; spatio-temporal decomposition operation scheme; spatio-temporal decomposition operation scheme (Systems-Centric Architecture, SCA); system integration operation scheme; missile control loop architecture optimisation scheme; SCA system architecture model; class association operation model; functional structure synthesis operation model.
- Author Biographies
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- 2024-06-30
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- AIR DEFENSE SYSTEMS
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Copyright (c) 2024 Анатолій Скорик,Олег Галицький,Олексій Звєрєв,Олексій Головін,Андрій Орлянський

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