L.V. Savkin - Post-graduate Student, Chief of Radio-Electronic Technique Bureau, Federal Enterprise «Lavochkin Association». E-mail: android4.1@mail.ru

In operation the method of creation system of functional and parametric monitoring and diagnostics of the spacecraft onboard control complex (OCC) on the basis of three fragments of uniform reconfigurable computing field interacting among themselves is offered. In the first module processing of control and diagnostic information and formation of the spacecraft OCC tests is carried out. The second module represents the homogeneous memorable environment and is intended for storage of values reference signatures. The third module exercises control of interaction between the first two modules and is intended for formation vector of technical condition OCC and vector of error diagnostic model. The first two modules represent the executive level of control and diagnostic system. The third module represents the controlling level and level of decision-making. The organization of functional and parametric monitoring and diagnostics of spacecraft OCC is defined by algorithm of interaction between these modules. The structural organization is given and the general principles of functioning the triplex reconfigurable system of functional and pa-rametric monitoring and diagnostics spacecraft OCC are considered.

 

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