Automatic switching control method of hot-standby redundancy of remote control computer

A technology of remote control and control method, which is applied in general control system, control/adjustment system, instrument, etc., can solve serious problems, hidden dangers of misoperation, misoperation and other problems, and achieve the effect of improving switching efficiency and high timeliness

Inactive Publication Date: 2017-10-17
BEIJING INST OF SPACE LAUNCH TECH +1
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Problems solved by technology

[0004] For the manual switching method, when a fault occurs, the operator needs to confirm the fault phenomenon first, and then manually switch on the operation man-machine interface. It is necessary to specify the judgment standard in advance and need to have a decision whether to switch. The efficiency of manual judgment is relatively low;
[0005] For the method of complete dual-machine hot backup, both machines have monitoring and control functions at the same time. In this method, there is no switching time, and the two machines can be seamlessly switched. However, since the two machines have control functions at the same time, it may introduce the risk of misuse The possibility of operation and the hidden dangers are more serious, so the method of complete dual-system hot backup also has certain risks

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  • Automatic switching control method of hot-standby redundancy of remote control computer
  • Automatic switching control method of hot-standby redundancy of remote control computer

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Embodiment Construction

[0024] The present invention is a remote control computer hot-standby automatic switching control method suitable for various failure modes, which is applied to the ground measurement and launch control process of a carrier rocket, and realizes the hot-standby redundancy switching of the remote control computer during long-distance testing. First, the hardware of the two mutually redundant remote control computers is equipped with dual network cards, and can be bundled through INTEL's Team technology, using only one IP address externally, and forming a network through dual redundant Ethernet switches; Both remote control computers can publish network variables through Ethernet, realize mutual monitoring function, and communicate with programmable logic controller PLC through Ethernet; again, one of the two remote control computers has a monitoring programmable logic controller. The function of PLC status, and the other one has the function of monitoring the PLC status of the pr...

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Abstract

The invention relates to an automatic switching control method of hot-standby redundancy of a remote control computer. The method is applied to a ground measurement-launch-control flow of a launch vehicle to realize hot-standby redundancy switching of a remote control computer during long-distance testing. Hardware units of two re mote control computers redundant to each other are equipped with dual-network cards, dual-network card binding is carried out by an INTEL Team technique and only one IP address is used externally, and a network is formed by a dual-machine-redundant Ethernet switch. The two remote control computers can issue network variables by the Ethernet network to realize a mutual monitoring function; and data communication is carried out by the Ethernet network and a programmable logic controller (PLC). When a fault occurs at one remote control computer, the other remote control computer monitors the state of the fault remote control computer and the current control state of the fault computer is synchronized to the other fault-free computer automatically, so that automatic switching control is realized.

Description

technical field [0001] The invention belongs to the field of test control of carrier rocket ground equipment, and designs a remote control computer hot backup redundant automatic switching control method. Background technique [0002] In the ground test process of the launch vehicle, the control computer is set in the test and launch control room to test and control the launch vehicle remotely. Therefore, the control interaction between the remote control computer and the programmable logic controller (PLC) at the front end of the launch position of the launch vehicle is very important. . [0003] Due to the requirements of system reliability, etc., the remote control computer is generally a dual-machine hot-standby redundant mode, because the prior art does not have a general fault detection redundancy switching method for PCs; therefore, the remote control computer is hot-standby redundant. The redundant switching in the remaining method is generally divided into three me...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B9/03
CPCG05B9/03
Inventor 郑国昆苏娟刘丽媛刘杰奇许学雷
Owner BEIJING INST OF SPACE LAUNCH TECH
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