FIELD: physics, computer engineering.
SUBSTANCE: invention relates to computer engineering and can be used in designing strapdown inertial reference systems which are part of automatic control systems for highly-manoeuvrable ships, aircraft, space rockets and spacecraft in particular, as well as mobile robotic systems which are characterised by operability in extreme conditions. The device includes a microprogramme control unit, two matrix neuroprocessor units, an operational device, matrix memory, a secondary power source, a communication unit, authorised access memory and an environment sensor.
EFFECT: faster matrix computations.
23 cl, 20 dwg
Title | Year | Author | Number |
---|---|---|---|
INERTIAL STRAPDOWN SYSTEM | 2013 |
|
RU2563333C2 |
COMPUTER SYSTEM | 2013 |
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RU2536434C2 |
FAILURE-FREE COMPUTING SYSTEM | 2013 |
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RU2541839C2 |
HIGHWAY-MODULAR COMPUTER SYSTEM | 2013 |
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RU2564626C2 |
AUTOMATIC CONTROL SYSTEM | 2013 |
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RU2534955C1 |
SPACECRAFT CONTROL SYSTEM | 2013 |
|
RU2560204C2 |
ASTRONAVIGATION SYSTEM | 2013 |
|
RU2548927C1 |
DATA TRANSMISSION CONTROLLER | 2013 |
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RU2514135C1 |
PROCESS CONTROL COMPUTER | 2013 |
|
RU2563139C2 |
NEUROPROCESSOR | 2011 |
|
RU2473126C1 |
Authors
Dates
2015-06-10—Published
2013-08-23—Filed