箭载应答机测试系统及监控软件设计
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摘要
20世纪末,航天测控技术的发展进入了一个高潮。航天测控技术是当代高新科技的一个重要领域。国内外测控技术发展的历程表明,测控技术是与卫星技术、运载器技术以及载人航天技术等同步协调发展的。最能集中展现测控技术的航天测控系统是航天工程的重要组成部分,它既是火箭,航天运载器及其发射、在轨、返回段的重要支持保障系统,又是运行大回路中的重要环节。
航天测控系统主要包括飞行器测控系统和地面外安系统。外安系统,即无线电外弹道测量及靶场安全控制系统,包括箭上设备(主要是箭载应答机)、地面测量控制站和靶场测试设备三部分。其中,应答机作为应答式无线电测控系统箭载合作设备,安装于各类飞行器上,用于完成地面雷达上行信号的接收、处理,向测控雷达发送下行信号,实现测控系统上下行信号的转接功能,是实现高精度轨道测量的关键设备。箭载应答机作为地面测量控制站重要组成部分,建立一种精确、高效的应答机测试系统成为解决发射前应答机测试的重要内容。
应答机测试系统是外安系统地面测量控制站的主要组成部分。应答机测试系统由信息采集分机、信道分机、信号处理分机以及常用仪器组成,与地面控制台及光传输系统一起配合工作完成箭载应答机的单机功能测试和联机系统功能测试。
论文首先介绍了当前国内外航天测控技术的发展概况。在此基础上对箭载应答机进行了介绍。论文在介绍外安系统的组成及各个组成部分的基本功能的基础上,重点设计并完成了测速应答机、测距应答机和逃逸接收机在内的三种箭载应答机的单元测试和系统联试。
论文对应答机测试系统的硬件组成和软件设计进行了详细介绍。系统硬件设计采用模块化的设计方法,三种应答机的测试系统都是由信息采集分机、信道分机、信号处理分机等模块组成。论文以测速应答机测试系统为例,对各个功能模块的组成和性能指标的设计要求进行了详细介绍。软件的设计部分重点解决了总线信息实时处理与监控系统的实现问题,编写了各个软件模块的程序。此外,结合实际探讨了人机界面的设计原则与方法,并编程实现了人机交互界面。
应答机测试系统在针对包括测速应答机在内的三种应答机的系统测试中,达到了预期设计的各项要求。进一步的测试工作还在进行。
In the end of the 20th century, the development of the space monitoring and controlling technology had reached a climax. The Space monitoring and controlling technology is an important high-tech flied. By viewing the development of the domestic and international space extracting course, it can be concluded that space monitoring and controlling is improving along with missile technology, satellite technology, transportation technology, as well as manned spacecraft technology. As a significant part of the missile launching test and spacecraft engineering, the measuring and controlling system for spacecraft is not only the critical supporting and safeguarding system for the missile and launch vehicle, also play a significant role in the whole system.
The space monitoring and controlling system consists of aerocraft measuring system and the outside ballistic measuring and safe-controlling system. The outside ballistic measuring and safe-controlling system consists of devices on board, the ground controlling station and division safe-controlling system. Responders is the most familiar device on board, which is a wireless device for receiving up data and send it back after certain process to realize high-precision measurement. As an important part of the ground controlling station, to gesign an effective measuring system for responders before launching is a critical subject.
The monitoring system of responding beacons (RSP) on board is the main part of the outside ballistic measuring and safe-controlling system. The system consists by the information collecting subsystem, the data channel subsysrem, the signal processing subsystem and universal apparatuses. By working with ground console and the optical transporting system, the system can accomplish the testing of capacity index and system function.
First of all, the paper introduced the general situation of the domestic and international development of space monitoring and controlling technology, especially the outside ballistic measuring techniques. Then, the responding beacons are particularly discussed. The paper also introduced the consisting strunture of the outside ballistic measuring and safe-controlling system and the function of each part, and designed and accomplished the monitoring system for three main responding beacons on board.
The paper gives a full description of the structure of the hardware and the designing method of the monitoring software. The whole system is built based on the module method.Taking speed measuring system as example, the paper discussed the principle of every module.The monitoring software focused on the real-time disposing of the bus data, the software modules are accomplished based on it.Besides, according to the engineering and practial guide, a friendly operational HMI(Human Machine Interface) is presented in the paper.
The system in the paper has qualified for the prospective requirements, the more testing method will be implemented until the system meets all the qualifications.
航天测控系统主要包括飞行器测控系统和地面外安系统。外安系统,即无线电外弹道测量及靶场安全控制系统,包括箭上设备(主要是箭载应答机)、地面测量控制站和靶场测试设备三部分。其中,应答机作为应答式无线电测控系统箭载合作设备,安装于各类飞行器上,用于完成地面雷达上行信号的接收、处理,向测控雷达发送下行信号,实现测控系统上下行信号的转接功能,是实现高精度轨道测量的关键设备。箭载应答机作为地面测量控制站重要组成部分,建立一种精确、高效的应答机测试系统成为解决发射前应答机测试的重要内容。
应答机测试系统是外安系统地面测量控制站的主要组成部分。应答机测试系统由信息采集分机、信道分机、信号处理分机以及常用仪器组成,与地面控制台及光传输系统一起配合工作完成箭载应答机的单机功能测试和联机系统功能测试。
论文首先介绍了当前国内外航天测控技术的发展概况。在此基础上对箭载应答机进行了介绍。论文在介绍外安系统的组成及各个组成部分的基本功能的基础上,重点设计并完成了测速应答机、测距应答机和逃逸接收机在内的三种箭载应答机的单元测试和系统联试。
论文对应答机测试系统的硬件组成和软件设计进行了详细介绍。系统硬件设计采用模块化的设计方法,三种应答机的测试系统都是由信息采集分机、信道分机、信号处理分机等模块组成。论文以测速应答机测试系统为例,对各个功能模块的组成和性能指标的设计要求进行了详细介绍。软件的设计部分重点解决了总线信息实时处理与监控系统的实现问题,编写了各个软件模块的程序。此外,结合实际探讨了人机界面的设计原则与方法,并编程实现了人机交互界面。
应答机测试系统在针对包括测速应答机在内的三种应答机的系统测试中,达到了预期设计的各项要求。进一步的测试工作还在进行。
In the end of the 20th century, the development of the space monitoring and controlling technology had reached a climax. The Space monitoring and controlling technology is an important high-tech flied. By viewing the development of the domestic and international space extracting course, it can be concluded that space monitoring and controlling is improving along with missile technology, satellite technology, transportation technology, as well as manned spacecraft technology. As a significant part of the missile launching test and spacecraft engineering, the measuring and controlling system for spacecraft is not only the critical supporting and safeguarding system for the missile and launch vehicle, also play a significant role in the whole system.
The space monitoring and controlling system consists of aerocraft measuring system and the outside ballistic measuring and safe-controlling system. The outside ballistic measuring and safe-controlling system consists of devices on board, the ground controlling station and division safe-controlling system. Responders is the most familiar device on board, which is a wireless device for receiving up data and send it back after certain process to realize high-precision measurement. As an important part of the ground controlling station, to gesign an effective measuring system for responders before launching is a critical subject.
The monitoring system of responding beacons (RSP) on board is the main part of the outside ballistic measuring and safe-controlling system. The system consists by the information collecting subsystem, the data channel subsysrem, the signal processing subsystem and universal apparatuses. By working with ground console and the optical transporting system, the system can accomplish the testing of capacity index and system function.
First of all, the paper introduced the general situation of the domestic and international development of space monitoring and controlling technology, especially the outside ballistic measuring techniques. Then, the responding beacons are particularly discussed. The paper also introduced the consisting strunture of the outside ballistic measuring and safe-controlling system and the function of each part, and designed and accomplished the monitoring system for three main responding beacons on board.
The paper gives a full description of the structure of the hardware and the designing method of the monitoring software. The whole system is built based on the module method.Taking speed measuring system as example, the paper discussed the principle of every module.The monitoring software focused on the real-time disposing of the bus data, the software modules are accomplished based on it.Besides, according to the engineering and practial guide, a friendly operational HMI(Human Machine Interface) is presented in the paper.
The system in the paper has qualified for the prospective requirements, the more testing method will be implemented until the system meets all the qualifications.
引文
[1]刘竹生等.CZ-2F运载火箭技术手册.北京航天部一院一部技术文件.1989
[2]吴立勋.外测与安全系统:导弹与航天丛书-液体弹道导弹与运载火箭系统.北京宇航出版社.1993
[3]马昕晖,蔡远文,盖江南.运载火箭外测安全系统地面测试设备仿真训练系统[J].指挥技术学院学报.2001.8.
[4]陈方允.卫星测控手册.北京:科学出版社,1992
[5]石书济.飞行器测控系统.看不见的领航员[M].国防工业出版社.2001.417-54.
[6]张旭辉.CZ-2F火箭遥测仿真系统[J].导航与航天运载技术.2004.1
[7]宋建强,曾贵明.CZ-2F外测安全系统地面无线测试设备研制任务书.北京:航天一院一部技术文件.1998
[8]巫幪,苏涛,史佳欢.通用信号处理板卡的CPCI总线接口设计和驱动开发.国外电子元器件.2007.02
[9]李坡,孙茂阳,王伟,陈曾平.一种基于CPCI总线的红外图像采集卡[J];现代电子技术:2004
[10]董圆.CPCI—开放式工控机制胜的关键[J.江苏科技报.2003
[11]解英杰,邵剑峰.CompactPCI在CTI领域中的应用[J];通信产业报.2003
[12]Advantest R3132 Series Spectrum Analyzer Operation Manual.1999410-462
[13]王婷,王俊.基于GPIB的自动测试系统设计[J],电子测量技术.2007.5.
[14]王洪林.基于GPIB接口的自动测试系统在射频测试中的应用[J].舰舶电子对抗.2007.6.
[15]杜诚谦,潘洁伦.新一代运载火箭地面测试发控系统一体化设计概述.航天控制[J].2004.2
[16]陈钰.GPIB系统中光功率计自动测试的实现[J].微计算机信息.2007.3.
[17]冯慧,刘建坤,周伟超.基于Windows环境的GPIB接口设计实现[J].测控技术.2000.19
[18]蒋建虎,韩英.工业以太网技术的现状和发展[J].洛阳工业高等专科学校学报.2005.6
[19]张厥盛,郑继禹,万心平.锁相技术IM].西安电子科技大学出版社.2003.1.
[20]刘路放.Visual C++与面向对象程序设计教程[M].北京:高等教育出版社.2002.3.
[21]郑莉,董渊.C++语言程序设计(第2版).清华大学出版社,2001.8
[22]彭道刚,杨平.基于VC++数据采集监控系统设计[J].第六届工业仪表与自动化学术会议论文集.
[23]相参应答机技术说明书及测试细则.电子科技集团公司第十研究所技术文件.1997
[24]应答机单元测试台技术说明书.电子科技集团公司第十研究所技术文件.1998
[25]应答机测试发射机技术说明书.电子科技集团公司第十研究所技术文件.1998
[26]张江岳,张全金,乔春丽,卢学新.基于GPIB接口的频谱分析仪CAM/CAT系统的开发与应用[J].中国电子科技集团公司四十一研究所.
[27]闫高伟,谢刚,王红兵.带GPIB接口的数字信号频率源设计[J].电子测量与仪器学报增刊.2002
[28]付平,李静.PCI-GPIB卡VISA库设计.电子测量与仪器学报增刊.2002
[29]黄学祥.利用近地卫星鉴定航天测控设备外测精度的方法研究.飞行器测控学报.2001.01
[30]吴斌,刘利生,黄永宣;.航天测控网测量体制的改进探讨[J];电讯技术:2003.03
[31]徐皑冬,王宏,杨志家.基于以太网的工业控制网络[J];信息与控制;2000.02
[32]马克刚.工业以太网在网络控制系统中的应用研究[D];合肥工业大学;2005.
[33]Lee K C,Lee S;Performance evaluation of switched Ethemet for real-time industrial communications[M];Computer Standards &Interfaces;2002
[34]Babb M;The race for real time Ethemet[M];Computing &Control Engineering;2004
[35]廖天发,王国荣,李国进,钟继光.VC++串口通信在水下焊接远程控制中的应用[J];焊接技术;2004.01
[36]马瑞萍,罗刚,邓志渊,李小群.基于VC++语言的HP34401A串口远程控制实现[J].微计算机信息.2004.09
[37]鞠儒生,王辉,陈燕.VC++中实现基于多线程的串行通讯[J].计算机测量与控制:2002.01
[38]王海红,李万山,苟玉君.利用MSComm控件实现微机与GPS-OEM板的串口通信.2000中国控制与决策学术年会论文集[C].2000
[39]王振友,宗风强.在Visual Basic6.0下实现组态王与单片机的串口通信;山东省计算机学会2005年信息技术与信息化研讨会论文集[C];2005
[40]刘君华,白鹏.基于LabWindows/CVI的虚拟仪器设计[M].北京:电子工业出版社,2003.
[41]季青.用VB实现基于GPIB的自动测试系统.江苏省计量测试学术论文集[C].2007
[42]Ward D A,Exon J La T;Using Rogowski Coils for Transient Current Measurements[M];Engineering Science and Education Journal;1993
[43]杨文杰.自动测试系统发展动向[J].微型机与应用.1997
[44]杨乐平 李海涛 虚拟仪器技术概论[M]电子工业出版社 2003.07
[45]Shayan Y R,Le-Ngoc T.All digital Phase-locked loop:concapts,design and applications[M];IEE Proceedings.1989
[46]William c Lindsey,Chak Ming Chie.A survey of digital phase-locked loops[M];Proceedings of the IEEE.1981
[47]徐跃,王奇,何秋阳.一种可编程的全数字锁相环路的实现[J];电子技术应用:2004.11
[48]黄锡滋.软件可靠性分配FMEA及FTA[J].质量与可靠性.1994.05
[49]申光耀.软件安全性保障框架及安全性技术应用[D].北京信息控制研究所.2005
[50]徐仁佐,肖英柏,向剑文.某通讯监控系统可靠性分配与验证[J];小型微型计算机系统.2000.08
[51]潘高泉.应答机自动测试系统及仿真测试方案[J];电讯技术.2007.12
[2]吴立勋.外测与安全系统:导弹与航天丛书-液体弹道导弹与运载火箭系统.北京宇航出版社.1993
[3]马昕晖,蔡远文,盖江南.运载火箭外测安全系统地面测试设备仿真训练系统[J].指挥技术学院学报.2001.8.
[4]陈方允.卫星测控手册.北京:科学出版社,1992
[5]石书济.飞行器测控系统.看不见的领航员[M].国防工业出版社.2001.417-54.
[6]张旭辉.CZ-2F火箭遥测仿真系统[J].导航与航天运载技术.2004.1
[7]宋建强,曾贵明.CZ-2F外测安全系统地面无线测试设备研制任务书.北京:航天一院一部技术文件.1998
[8]巫幪,苏涛,史佳欢.通用信号处理板卡的CPCI总线接口设计和驱动开发.国外电子元器件.2007.02
[9]李坡,孙茂阳,王伟,陈曾平.一种基于CPCI总线的红外图像采集卡[J];现代电子技术:2004
[10]董圆.CPCI—开放式工控机制胜的关键[J.江苏科技报.2003
[11]解英杰,邵剑峰.CompactPCI在CTI领域中的应用[J];通信产业报.2003
[12]Advantest R3132 Series Spectrum Analyzer Operation Manual.1999410-462
[13]王婷,王俊.基于GPIB的自动测试系统设计[J],电子测量技术.2007.5.
[14]王洪林.基于GPIB接口的自动测试系统在射频测试中的应用[J].舰舶电子对抗.2007.6.
[15]杜诚谦,潘洁伦.新一代运载火箭地面测试发控系统一体化设计概述.航天控制[J].2004.2
[16]陈钰.GPIB系统中光功率计自动测试的实现[J].微计算机信息.2007.3.
[17]冯慧,刘建坤,周伟超.基于Windows环境的GPIB接口设计实现[J].测控技术.2000.19
[18]蒋建虎,韩英.工业以太网技术的现状和发展[J].洛阳工业高等专科学校学报.2005.6
[19]张厥盛,郑继禹,万心平.锁相技术IM].西安电子科技大学出版社.2003.1.
[20]刘路放.Visual C++与面向对象程序设计教程[M].北京:高等教育出版社.2002.3.
[21]郑莉,董渊.C++语言程序设计(第2版).清华大学出版社,2001.8
[22]彭道刚,杨平.基于VC++数据采集监控系统设计[J].第六届工业仪表与自动化学术会议论文集.
[23]相参应答机技术说明书及测试细则.电子科技集团公司第十研究所技术文件.1997
[24]应答机单元测试台技术说明书.电子科技集团公司第十研究所技术文件.1998
[25]应答机测试发射机技术说明书.电子科技集团公司第十研究所技术文件.1998
[26]张江岳,张全金,乔春丽,卢学新.基于GPIB接口的频谱分析仪CAM/CAT系统的开发与应用[J].中国电子科技集团公司四十一研究所.
[27]闫高伟,谢刚,王红兵.带GPIB接口的数字信号频率源设计[J].电子测量与仪器学报增刊.2002
[28]付平,李静.PCI-GPIB卡VISA库设计.电子测量与仪器学报增刊.2002
[29]黄学祥.利用近地卫星鉴定航天测控设备外测精度的方法研究.飞行器测控学报.2001.01
[30]吴斌,刘利生,黄永宣;.航天测控网测量体制的改进探讨[J];电讯技术:2003.03
[31]徐皑冬,王宏,杨志家.基于以太网的工业控制网络[J];信息与控制;2000.02
[32]马克刚.工业以太网在网络控制系统中的应用研究[D];合肥工业大学;2005.
[33]Lee K C,Lee S;Performance evaluation of switched Ethemet for real-time industrial communications[M];Computer Standards &Interfaces;2002
[34]Babb M;The race for real time Ethemet[M];Computing &Control Engineering;2004
[35]廖天发,王国荣,李国进,钟继光.VC++串口通信在水下焊接远程控制中的应用[J];焊接技术;2004.01
[36]马瑞萍,罗刚,邓志渊,李小群.基于VC++语言的HP34401A串口远程控制实现[J].微计算机信息.2004.09
[37]鞠儒生,王辉,陈燕.VC++中实现基于多线程的串行通讯[J].计算机测量与控制:2002.01
[38]王海红,李万山,苟玉君.利用MSComm控件实现微机与GPS-OEM板的串口通信.2000中国控制与决策学术年会论文集[C].2000
[39]王振友,宗风强.在Visual Basic6.0下实现组态王与单片机的串口通信;山东省计算机学会2005年信息技术与信息化研讨会论文集[C];2005
[40]刘君华,白鹏.基于LabWindows/CVI的虚拟仪器设计[M].北京:电子工业出版社,2003.
[41]季青.用VB实现基于GPIB的自动测试系统.江苏省计量测试学术论文集[C].2007
[42]Ward D A,Exon J La T;Using Rogowski Coils for Transient Current Measurements[M];Engineering Science and Education Journal;1993
[43]杨文杰.自动测试系统发展动向[J].微型机与应用.1997
[44]杨乐平 李海涛 虚拟仪器技术概论[M]电子工业出版社 2003.07
[45]Shayan Y R,Le-Ngoc T.All digital Phase-locked loop:concapts,design and applications[M];IEE Proceedings.1989
[46]William c Lindsey,Chak Ming Chie.A survey of digital phase-locked loops[M];Proceedings of the IEEE.1981
[47]徐跃,王奇,何秋阳.一种可编程的全数字锁相环路的实现[J];电子技术应用:2004.11
[48]黄锡滋.软件可靠性分配FMEA及FTA[J].质量与可靠性.1994.05
[49]申光耀.软件安全性保障框架及安全性技术应用[D].北京信息控制研究所.2005
[50]徐仁佐,肖英柏,向剑文.某通讯监控系统可靠性分配与验证[J];小型微型计算机系统.2000.08
[51]潘高泉.应答机自动测试系统及仿真测试方案[J];电讯技术.2007.12