FIELD: information technology.
SUBSTANCE: invention can be used in designing computing means for systems for controlling highly manoeuvrable aviation and space-rocket objects where there is need for fast computation of functions, for example, trigonometric functions, used in matrix transformations when solving tasks of forming an inertial coordinate system based on information from angular velocity sensors, and when solving tasks for maintaining operating capacity of computers during changes in parameters of LSI elements due to the effect of natural or artificial ionising radiations. The device has a unit for communication with an on-board computer or which controls a higher level subsystem, a control device, a buffer register, a memory device, multipliers, an adder and an output register.
EFFECT: fewer faults in microchips.
5 cl, 5 dwg
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Authors
Dates
2013-01-20—Published
2011-10-28—Filed