Application of Decomposition Procedure for an Optimal Design of an Air-Defense Missile System and Its Components on Early Development Stages. Part Ⅱ

摘要

The development of the decomposition procedure for problems of optimal design of complex technical systems was suggested in [ 1 ]. In this paper, the application of a technique based on decomposition procedure is considered. The designed technique is used to form an air-defense missile system at the stage of technical proposals. The air-defense missile system is regarded as a complex hierarchical multilevel system. The statement of the design problem for the air-defense missile system, its subsystems, and components on individual hierarchical levels is given. The problem of a rational form of air-defense missile system, its subsystems, and components is formalized as a problem of structural and parametrical synthesis. The technique of decomposition and the corresponding algorithm described in [ 1 ] are applied to the solution of a design problem for the air-defense missile system. The iteration procedure of task interaction was developed for tasks solved on individual hierarchical levels. Vectors of constructive determining parameters optimized at every level are chosen. Methodical material is illustrated by numerical examples.