Triple-redundancy control computer and fault-tolerant control system

A control computer and triple-redundancy technology, applied in computer control, general control system, control/regulation system, etc., can solve problems such as reducing system real-time performance, increasing time overhead, increasing system software and hardware complexity, etc.

Active Publication Date: 2014-12-24
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

On the one hand, this technical solution increases the complexity of system software and hardware, on the other hand, it increases additional time overhead and reduces the real-time performance of the system.
In addition, in some control systems, such as aerospace vehicle control systems, there are strict constraints on the weight and power consumption of control system supporting equipment (which can be di...

Method used

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Embodiment

[0102] The control system of the present invention is introduced below by taking the carrier control system as an example, wherein the three-redundancy sensor equipment is three inertial measurement combinations, the double-redundancy sensor equipment is two GPS receivers, and the three-redundancy actuator is, for example, The main engine servo mechanism, the dual-redundancy actuator is, for example, the pneumatic rudder servo mechanism; the local switch value input signal is, for example, a take-off signal, and the local switch value power control command can be, for example, the pyrotechnic detonation power command, which is used for detonation distance triple redundancy The control computer is close to the pyrotechnics; the characteristic control instruction can be, for example, the deflection angle instruction of the main engine servo mechanism, which is only used for fault judgment of the backup machine; the digital continuous quantity control instruction of the actuator is...

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Abstract

The invention discloses a triple-redundancy control computer and a fault-tolerant control system. The triple-redundancy control computer comprises a switching value voting array module and three completely-independent sub-computers. The switching value voting array module receives switching value control signals output by the three sub-computers, backs up the switching value control signals, and outputs switching value power control instructions through a hardware voter. Each sub-computer determines a left computer and a right computer which correspond to the sub-computer according to a left and right computer role definition table. Each sub-computer comprises a synchronous module, a self-detection module, a left computer detection module, a right computer detection module, a duty control module, a host module and a switching value control output module. According to the triple-redundancy control computer and the fault-tolerant control system, on the basis of meeting the requirement of the system for hard real-time performance, more single-computer fault modes can be tolerated, the overall high reliability of the system is improved, and the software and hardware expenses are reduced.

Description

technical field [0001] The invention relates to a triple redundant control computer and a fault-tolerant control system. Background technique [0002] Under the condition of certain reliability level of components and stand-alone products, redundant fault-tolerant technology is usually used to improve the overall reliability of the computer control system, such as dual-machine backup / dual-mode redundancy, triple-mode redundancy (TMR) and other redundancy technologies have been It is widely used in aircraft control systems with high reliability requirements. [0003] The dual-mode redundant system improves system reliability by adding a set of homogeneous hardware devices. The general technical solution is that the two machines collect data synchronously, process the data, and generate data output at the same time and send it to the voting device for comparison of the output data: when the output data results of the two machines are the same, it indicates that the system is ...

Claims

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Application Information

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IPC IPC(8): G05B19/048
Inventor 黄波刘学士张福鑫刘俊阳刘茜筠曹帮林陈伟
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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