FIELD: physics, control.
SUBSTANCE: invention relates to automatics and may be used in development of control systems of aviation objects, items of rocket-space engineering and robotic complexes operating under extreme conditions (wide range of temperature variation from -60 to +125°C, mechanical impact in the form of strikes and wideband vibration) in ionising radiation fields. The proposed system comprises actuating elements of a control object, an angular speed sensor, an acceleration sensor, an information collection unit, satellite navigation equipment, an inertial navigation subsystem, control computing devices, a sensor of external impact, a blocking signal generator, a memory with authorized access and actuating elements, a power supply subsystem, an image processing subsystem, a control unit and an optical correction subsystem.
EFFECT: improved efficiency of control system operation, namely, preservation of operability in case of any single failure in system equipment, and also preservation of functioning and accuracy of control in case of parametric changes in components caused by ageing, change of environmental temperature and dose factors of ionising radiation.
24 cl, 24 dwg
Title | Year | Author | Number |
---|---|---|---|
INERTIAL STRAPDOWN SYSTEM | 2013 |
|
RU2563333C2 |
ASTRONAVIGATION SYSTEM | 2013 |
|
RU2548927C1 |
SPACECRAFT CONTROL SYSTEM | 2013 |
|
RU2560204C2 |
NEUROCOMPUTER | 2013 |
|
RU2553098C2 |
HIGHWAY-MODULAR COMPUTER SYSTEM | 2013 |
|
RU2564626C2 |
COMPUTER SYSTEM | 2013 |
|
RU2536434C2 |
FAILURE-FREE COMPUTING SYSTEM | 2013 |
|
RU2541839C2 |
HARDWARE AND SOFTWARE DEBUGGING SIMULATION SYSTEM | 2013 |
|
RU2516703C1 |
PROCESS CONTROL COMPUTER | 2013 |
|
RU2563139C2 |
AUTOMATIC CONTROL SYSTEM | 2011 |
|
RU2494006C2 |
Authors
Dates
2014-12-10—Published
2013-04-09—Filed