Functional-parametric configuration of the onboard computer system of the spacecraft based on the prediction of its degradation

The decision of questions of operational autonomous control onboard computer systems of spacecrafts by means of a flexible control modes of components and dispatching computational process requires a rational choice of their configuration in order to achieve the maximum beneficial effect from the target system. Developed approach is functional-parametric reconfiguration onboard computer systems of spacecrafts through the operational management structure of the tasks and operational parameters of the elements of the structure-based prediction of its state, including analysis of the system resource and the conditions of its functioning. It can be used in the development of algorithms for operational autonomous reconfiguration of the onboard computer systems of promising specialized spacecrafts operating under the influence of adverse factors of different origin.