CN202918339U - Ground test-launch-control system of carrier rocket based on cloud computing - Google Patents
Ground test-launch-control system of carrier rocket based on cloud computing Download PDFInfo
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- CN202918339U CN202918339U CN 201220297002 CN201220297002U CN202918339U CN 202918339 U CN202918339 U CN 202918339U CN 201220297002 CN201220297002 CN 201220297002 CN 201220297002 U CN201220297002 U CN 201220297002U CN 202918339 U CN202918339 U CN 202918339U
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Abstract
The utility model discloses a ground test-launch-control system of a carrier rocket based on cloud computing. The system comprises a data collection terminal, a cloud computing server and a data processing terminal. The data collection terminal is used for receiving data of subsystems of the carrier rocket and sending the data to the cloud computing server through a transmission network; a logged-in user at the data processing terminal operates on the data, and the data processing terminal sends a resource request and an operation request to the cloud computing server according to the operation of the logged-in user; and the cloud computing server includes processing resources used for processing the data and is used for applying for processing resources according to the resource request and the operation request which are received from the data processing terminal, processing the data sent by the data collection terminal according to the operation request and sending processing result data back to the data processing terminal through the transmission network. According to the utility model, the problems of low equipment utilization rate and difficult information security guaranteeing caused by independent management of an original carrier rocket ground test-launch-control system on the computation of the subsystems are overcome.
Description
Technical field
The invention belongs to carrier rocket and survey control techniques field, particularly an a kind of carrier rocket ground launch vehicle measurement based on cloud computing.
Background technology
The ground launch vehicle measurement of China's active service carrier rocket is by front end data collection terminal, multimedia multi-screen surveillance, master control net, each system's Back end data processing terminal of the subsystems such as dynamical system, control system, measuring system, emission back-up system and spare system and comprehensively send out control system etc. and partly form.Each subsystem front end data collection terminal comprises dynamical system, control system, measuring system etc., and the process and the result data that produce when these subsystems are worked self send to the rear end in real time by the master control net, monitors the rocket state for the staff.The master control net of launch vehicle measurement is comprised of server, switch, many work stations and network monitoring device, when using twisted-pair feeder to carry out exchanges data between each hardware, and can also be to transfer of data monitoring performance, detection.For having guaranteed data transmission quality and reliability, system also utilize the media implementation such as optical fiber to test data, send out the long-distance transmissions of the data such as control instruction, video analog signal.A comprehensive control system is responsible for distribution and controls, sends the tasks such as control command (firing order and emergency cutoff instruction).
At present, because it is numerous that a control subsystem is surveyed on carrier rocket ground, make launch vehicle measurement face lot of challenges, such as the challenge of overlapping together the uneven testing progress aspect that causes of time owing to each subsystem equipment, because the challenge of the secure context that the dispersed management of each subsystem equipment causes, and because each subsystem is responsible for the challenge of the cost aspect that equipment of itself buying, test and maintenance support cause.
Summary of the invention
Technology of the present invention is dealt with problems and is: a kind of carrier rocket ground launch vehicle measurement based on cloud computing is provided, has overcome original carrier rocket ground launch vehicle measurement each subsystem computing is managed independently the problem that the utilization rate of equipment and installations of bringing is low, information security is difficult to guarantee.
Technical solution of the present invention is:
A kind of carrier rocket ground launch vehicle measurement based on cloud computing comprises: data collector terminal, cloud computing server, data processing terminal.
Described data collector terminal is used for receiving test data, control instruction and the quantity of state data of carrier rocket front end dynamical system, control system, measuring system, and sends to described cloud computing server by transmission network;
Described data processing terminal is operated described test data, a control instruction and quantity of state data by login user, and sends resource request and operation requests according to the operation of login user to described cloud computing server;
Described cloud computing server comprises the processing resource that described test data, a control instruction and quantity of state data are processed, according to the resource request that comes from described data processing terminal and the operation requests that receive, resource is processed in application, and utilize to process test data that resource sends described data collector terminal according to operation requests, send out the control instruction and the quantity of state data are processed, and the result data communication device is crossed transmission network turn back to described data processing terminal.
Further, described transmission resource request is processed resource by the data collector terminal to the cloud computing server application, described processing resource comprises CPU check figure, internal memory, hard disk and operating system, and by described cloud computing server according to processing the resource construction virtual processor, obtain test data from described data collector terminal, send out control instruction and quantity of state data and process according to operation requests by described virtual processor.
Further, described transmission network is optical fiber transmission network.
The present invention compared with prior art has following advantage:
The present invention surveys calculating and the storage resources unification of sending out each subsystem of control by cloud computing technology with ground and manages, and utilizes cloud computing server that calculation resources is carried out unified management, has reduced each subsystem terminal quantity and maintenance cost; On cloud computing server, take virtual machine as processing unit according to the operation requests of data processing terminal to being processed by the place ahead data of each collected subsystem of data collector terminal.When the inadequate resource of cloud computing server, only need the simple server hardware resource of adding just can carry out real-time migration to business, the work of each subsystem does not have any impact.If hardware resource is sufficient, then can use the highly reliable technology in virtual that each subsystem is carried out hot backup redundancy, improved the reliability of system.
The cloud platform all can be controlled the hardware interface of each subsystem terminal, whether is arranged, is authorized by the opening of cloud platform to hardware interface, has reduced the possibility of being introduced wooden horse, virus by each subsystem.Thoroughly solved because the virus that each subsystem terminal Decentralization causes and data leak threaten, guaranteed the information security of ground launch vehicle measurement.
Description of drawings
Fig. 1 is schematic diagram of the present invention;
Fig. 2 is cloud platform management software architecture diagram.
Embodiment
Below just by reference to the accompanying drawings the present invention is done further introduction.
Be illustrated in figure 1 as embodiment of the invention system schematic.Data collector terminal, cloud computing server, data processing terminal, network monitoring terminal, data storage server and input information output services station.Data processing terminal among Fig. 1 adopts the form of thin-client, use Intel Virtualization Technology to each in the cloud computing server, with the calculation resources unified management of original each subsystem of carrier rocket in cloud computing server, present embodiment adopts two cloud computing servers, but according to the operand of whole ground launch vehicle measurement also can be by increasing cloud computing server quantity to satisfy the Practical Calculation demand.
Data processing terminal is by sending resource request and operation requests to cloud computing server, and realization is mutual to cloud computing server.The Various types of data collected according to pending data collector terminal, but login user data processing terminal sends resource request to cloud computing server, receive can fictionalizing at cloud computing server of resource request and a plurality ofly can be formulated by the user virtual machine of configuration, the configuration of virtual machine is determined by indexs such as CPU check figure entrained in the resource request, internal memory, hard disk, OS Types.Virtual machine is managed by the cloud computing management software.The usefulness that logs on data processing terminal can get final product by according to original mode of operation the data of being collected by the data collector terminal being processed, thereby can guarantee the unified management to calculation resources, and has guaranteed that the user can't touch outside virus or wooden horse.
Further utilize the input information output services station of present embodiment, can be so that the user needs mounting software or during from outside import information, the realization external information swinging in or showing to internal information, has avoided because the safety issue that the dispersed management of each subsystem equipment causes.In cloud computing server constructed go out corresponding to each subsystem virtual machine and by the data message operating system that produces after the virtual machine computing and data message will real-time storage in data storage server.When again logging in after the user turns off the virtual machine of oneself, system can load the version of last stored automatically, thereby has guaranteed the safe and reliable of user data.
Moving management software at cloud computing server, be used for managing all resources of cloud computing server, the user meets the virtual machine that oneself requires according to the needs of oneself to the management software application.After getting the Green Light, just can generate the virtual machine of the customization operating system of virtual hardware.In fact, all virtual machines corresponding to data processing terminal all are to utilize physical resource common on the server.
The cloud computing management software is monitored the current resource using status of each virtual machine, farthest on average uses server resource, thereby server resource is the most reasonably utilized.
System operator can be realized supervision and management to whole platform by long-range management software, and the mode of utilizing iconic model represents the organizational structure of whole platform, and can be according to platform user's demand configuring virtual machine.And for the user, this platform is packaged, only needs by the use of Telnet pattern realization to virtual machine.
As shown in Figure 2, comprise 3 kinds of logic entities at cloud computing server: cloud computing management platform, node administration software and virtual machine VM.The effect of wherein cloud computing management platform is for the user provides a unified access interface, creates and generate VM, managing virtual disk mirroring.How many cloud computing servers are arranged in the system, only just can realize with the API that calls the user interface that the cloud computing management platform provides; Another effect is the node administration software in the management system, cloud computing server cluster namely, after receiving resource request, the cloud computing management platform can use resource allocation policy to start VM at the node administration software of correspondence, and the information that will newly create VM offers the user.The effect of node administration software is to calculate at cloud computing server, and the distribution of storage and Internet resources is to pay to the user in the mode of virtual machine in realization.Node administration software receives the scheduling of cloud computing management platform, and after the resource request of receiving the cloud computing management platform, node administration software can call local Virtual Machine Manager software creation VM, and VM information is sent to the cloud computing management platform registers.
Data processing terminal for the needs redundancy, on cloud computing server, can use the high reliability technology virtual machine of itself and this data processing terminal to be carried out the redundancy backup of active and standby virtual machine, delimit same hard disk areas store data between the two active and standby virtual machines, accelerated in the hostdown situation, spare machine recovers the time of calculating.
The unspecified part of the present invention belongs to general knowledge as well known to those skilled in the art.
Claims (3)
1. carrier rocket ground launch vehicle measurement based on cloud computing is characterized in that comprising: data collector terminal, cloud computing server, data processing terminal,
Described data collector terminal is used for receiving test data, control instruction and the quantity of state data of carrier rocket front end dynamical system, control system, measuring system, and sends to described cloud computing server by transmission network;
Described data processing terminal is operated described test data, a control instruction and quantity of state data by login user, and sends resource request and operation requests according to the operation of login user to described cloud computing server;
Described cloud computing server is processed resource according to the resource request application that comes from described data processing terminal that receives, and process test data that resource sends described data collector terminal, send out the control instruction and the quantity of state data are processed according to the operation requests utilization, and the result data communication device is crossed transmission network turn back to described data processing terminal.
2. a kind of carrier rocket ground launch vehicle measurement based on cloud computing as claimed in claim 1, it is characterized in that: described processing resource comprises CPU check figure, internal memory, hard disk and operating system, and by described cloud computing server according to processing the resource construction virtual processor, obtain test data from described data collector terminal, send out control instruction and quantity of state data and process according to operation requests by described virtual processor.
3. a kind of carrier rocket ground launch vehicle measurement based on cloud computing as claimed in claim 1, it is characterized in that: described transmission network is optical fiber transmission network.
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CN 201220297002 CN202918339U (en) | 2012-06-18 | 2012-06-18 | Ground test-launch-control system of carrier rocket based on cloud computing |
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Cited By (10)
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CN103487271A (en) * | 2013-09-24 | 2014-01-01 | 北京宇航系统工程研究所 | Fault diagnosis system of carrier rocket |
CN103592912A (en) * | 2013-10-30 | 2014-02-19 | 北京宇航系统工程研究所 | Distributed power measurement and control system applied to heavy carrier rocket |
CN103901864A (en) * | 2014-04-14 | 2014-07-02 | 上海航天电子通讯设备研究所 | Virtual console suitable for carrier rocket detecting, launching and control system |
CN104850452A (en) * | 2015-05-19 | 2015-08-19 | 北京宇航系统工程研究所 | High-reliability measurement, launch and control computing platform based on virtualization technology |
CN104991483A (en) * | 2015-05-19 | 2015-10-21 | 北京宇航系统工程研究所 | Test-launch-control remote monitoring platform based on virtualization technology |
CN105681311A (en) * | 2016-01-28 | 2016-06-15 | 北京宇航系统工程研究所 | Rocket ground network heterogeneous system based on cloud computing technology |
CN105739417A (en) * | 2016-05-06 | 2016-07-06 | 上海航天测控通信研究所 | Monitoring system and monitoring method capable of realizing customized monitoring of carrier rocket integral test-launch-control information |
CN106598060A (en) * | 2015-10-14 | 2017-04-26 | 上海宇航系统工程研究所 | Carrier rocket information integration electrical system |
CN107770100A (en) * | 2017-10-16 | 2018-03-06 | 中国运载火箭技术研究院 | One kind surveys hair control redundant network framework and redundancy approach |
CN109870070A (en) * | 2019-03-01 | 2019-06-11 | 北京星际荣耀空间科技有限公司 | A kind of integrated wireless launch vehicle measurement applied to Solid Launch Vehicle |
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- 2012-06-18 CN CN 201220297002 patent/CN202918339U/en not_active Expired - Lifetime
Cited By (17)
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CN103487271A (en) * | 2013-09-24 | 2014-01-01 | 北京宇航系统工程研究所 | Fault diagnosis system of carrier rocket |
CN103592912B (en) * | 2013-10-30 | 2015-10-21 | 北京宇航系统工程研究所 | A kind of distributed-power TT&C system being applied to heavy launcher |
CN103592912A (en) * | 2013-10-30 | 2014-02-19 | 北京宇航系统工程研究所 | Distributed power measurement and control system applied to heavy carrier rocket |
CN103901864B (en) * | 2014-04-14 | 2016-08-17 | 上海航天电子通讯设备研究所 | A kind of virtual control platform being applicable to carrier rocket launch vehicle measurement |
CN103901864A (en) * | 2014-04-14 | 2014-07-02 | 上海航天电子通讯设备研究所 | Virtual console suitable for carrier rocket detecting, launching and control system |
CN104991483B (en) * | 2015-05-19 | 2018-07-03 | 北京宇航系统工程研究所 | A kind of survey hair control remote monitoring platform based on virtualization technology |
CN104991483A (en) * | 2015-05-19 | 2015-10-21 | 北京宇航系统工程研究所 | Test-launch-control remote monitoring platform based on virtualization technology |
CN104850452A (en) * | 2015-05-19 | 2015-08-19 | 北京宇航系统工程研究所 | High-reliability measurement, launch and control computing platform based on virtualization technology |
CN106598060A (en) * | 2015-10-14 | 2017-04-26 | 上海宇航系统工程研究所 | Carrier rocket information integration electrical system |
CN106598060B (en) * | 2015-10-14 | 2020-02-28 | 上海宇航系统工程研究所 | Carrier rocket information integration electrical system |
CN105681311A (en) * | 2016-01-28 | 2016-06-15 | 北京宇航系统工程研究所 | Rocket ground network heterogeneous system based on cloud computing technology |
CN105681311B (en) * | 2016-01-28 | 2019-02-15 | 北京宇航系统工程研究所 | A kind of rocket ground network heterogeneous system based on cloud computing technology |
CN105739417A (en) * | 2016-05-06 | 2016-07-06 | 上海航天测控通信研究所 | Monitoring system and monitoring method capable of realizing customized monitoring of carrier rocket integral test-launch-control information |
CN105739417B (en) * | 2016-05-06 | 2018-03-16 | 上海航天测控通信研究所 | A kind of carrier rocket full surveys the monitoring system and its monitoring method of the customizable monitoring of hair control information |
CN107770100B (en) * | 2017-10-16 | 2019-12-20 | 中国运载火箭技术研究院 | Test, launch and control redundancy network architecture and redundancy method |
CN107770100A (en) * | 2017-10-16 | 2018-03-06 | 中国运载火箭技术研究院 | One kind surveys hair control redundant network framework and redundancy approach |
CN109870070A (en) * | 2019-03-01 | 2019-06-11 | 北京星际荣耀空间科技有限公司 | A kind of integrated wireless launch vehicle measurement applied to Solid Launch Vehicle |
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