可监测型数据记录系统的研制
摘要
随着航天事业的飞速发展,飞行器的发射也日趋频繁,必须设计一套可靠、有效的测试系统以确保它们的可靠发射及平稳运行。通过与无线电遥测系统比较,可监测型数据记录测试系统凭借其微型化、高速、抗过载和冲击、实时性等优点已经成为航天飞行器发射飞行试验中最为重要的测试方法,为飞行器的研制、发射、飞行试验及到后期的定型提供了重要的参考依据。
首先本文依据存储测试系统的原则,按照自顶向下的设计思想,对可监测型数据记录测试系统进行了总体设计,并详细分析了系统的工作方式和关键器件选型。然后本文详细介绍了采编存储器的组成原理、工作流程、硬件电路设计及关键器件的时序设计,提出了实时监测的设计思想,采用抽样式实时监测技术和混合数据流编码技术实现了实时监测与记录的同步,在存储器设计中,提出了“独立化”的思想,极大地提高了存储器的可靠性。接着叙述了地面测控台的设计思路、组成原理及工作流程,深入分析了可编程数字量信号源和长线传输等关键技术。
文章结论中给出了系统试验的实验数据,通过分析、比较远程读回的数据和信号源数据,证明该可控型数据记录系统能够可靠、准确地测试机上信号源的工作状态;除此以外通过分析从备用口读回的数据,发现该数据与远程读回的数据完全一致,从而证明了存储器可以在飞行器发射后取得真实的数据,并经过处理能够将记录的发射过程进行回放。
With the rapid development of space industry and the frequent firing of aerocraft, it is important to design a kind of reliable and effective test system to ensure the reliable firing and even running of aerocraft. Monitor Record Test System has been as the most important test measure in space aerocraft test for its micromation、high-speed、resistance to overload、resistance to impact and real-time, which provide important reference for the research and development of aerocraft、firing、flight experiment and the final approved product.
Firstly,integrated design of Monitor Record Test System was discussed in this paper, which is designed by the principle of memory and test system and top-down system, and the operation mode and flow of the system、the lectotype of key device by capacity calculation and performance analysis were also in this paper. Secondly, the paper introduced the composition principle、workflow、hardware circuits design and the sequential design of key device, put forward the idea of real-time monitor, and adopt the technology of sample real- real-time monitor and mixed coding to achieve the synchronization of monitor and data record; it presented the thought of“independent”in memory design, which improved the reliability of memory greatly. Thirdly, the design thought of test flat, and its composition principle、workflow were introduced, and the key technology of the programmed signal source and long-distance transmission were gone deep in to one by one.
The experimental data of the system test was discussed in the conclusion; it has been proved the Monitor Data Record Test System can test the active state of the signal source of aerocraft correctly and the reliably by analyzing or comparing the read-back data and signal source. What’s more, it has been proved the read-back data of spare port is same as the data of long range line after analyzing the data of spare port. Therefore, the memory can gain the true data after aerocraft firing and the firing process can be played back.
首先本文依据存储测试系统的原则,按照自顶向下的设计思想,对可监测型数据记录测试系统进行了总体设计,并详细分析了系统的工作方式和关键器件选型。然后本文详细介绍了采编存储器的组成原理、工作流程、硬件电路设计及关键器件的时序设计,提出了实时监测的设计思想,采用抽样式实时监测技术和混合数据流编码技术实现了实时监测与记录的同步,在存储器设计中,提出了“独立化”的思想,极大地提高了存储器的可靠性。接着叙述了地面测控台的设计思路、组成原理及工作流程,深入分析了可编程数字量信号源和长线传输等关键技术。
文章结论中给出了系统试验的实验数据,通过分析、比较远程读回的数据和信号源数据,证明该可控型数据记录系统能够可靠、准确地测试机上信号源的工作状态;除此以外通过分析从备用口读回的数据,发现该数据与远程读回的数据完全一致,从而证明了存储器可以在飞行器发射后取得真实的数据,并经过处理能够将记录的发射过程进行回放。
With the rapid development of space industry and the frequent firing of aerocraft, it is important to design a kind of reliable and effective test system to ensure the reliable firing and even running of aerocraft. Monitor Record Test System has been as the most important test measure in space aerocraft test for its micromation、high-speed、resistance to overload、resistance to impact and real-time, which provide important reference for the research and development of aerocraft、firing、flight experiment and the final approved product.
Firstly,integrated design of Monitor Record Test System was discussed in this paper, which is designed by the principle of memory and test system and top-down system, and the operation mode and flow of the system、the lectotype of key device by capacity calculation and performance analysis were also in this paper. Secondly, the paper introduced the composition principle、workflow、hardware circuits design and the sequential design of key device, put forward the idea of real-time monitor, and adopt the technology of sample real- real-time monitor and mixed coding to achieve the synchronization of monitor and data record; it presented the thought of“independent”in memory design, which improved the reliability of memory greatly. Thirdly, the design thought of test flat, and its composition principle、workflow were introduced, and the key technology of the programmed signal source and long-distance transmission were gone deep in to one by one.
The experimental data of the system test was discussed in the conclusion; it has been proved the Monitor Data Record Test System can test the active state of the signal source of aerocraft correctly and the reliably by analyzing or comparing the read-back data and signal source. What’s more, it has been proved the read-back data of spare port is same as the data of long range line after analyzing the data of spare port. Therefore, the memory can gain the true data after aerocraft firing and the firing process can be played back.
引文
[1]张文栋.存储测试系统的设计理论及其应用.北京:高等教育出版社,2002:10-150.
[2]Seakr Engineering Inc.s Products Specifications, www.seakr.com
[3]Calculex Inc.s Products Specifications,www.calculex.com
[4]Bruce Kaufman.A NonvolatileSolid-State Recorder for 100,000g.Environments. Sensors Magazine .Vol. 17, No. 6, June 2005, 46-51.
[5]Bruce Kaufman,On the use of COTS VME-based hardware to implement high performance recce solid state recorders,Proceedings of SPIE - The International Society for Optical Engineering,2006:155～160.
[6]Howard Johnson、Martin Graham,High-Speed Digital Design,Publishing House of Electronics Industry,2003:25～29.
[7]李开明.航天高密度大容量数据存储技术的发展.电子技术应。第 25卷,第4期,2000:45-48.
[8]史彦斌等.航空电子综合测试系统的发展现状及趋势.计量技术.第 29 卷,第 4 期,2004:75-80.
[9]王小东,郝志航.大容量固态存储技术.光学精密工程.第9 卷.第4 期,2001:396-400.
[10]Flash Databook, Samsung Corporation, 2007.
[11]李宁.数字合成信号源及高速数据采集测试平台的研究. 成都:国防工业出版社, 2004:21-36.
[12]张军,姚远,张其善.高速可编程 PCM 遥测帧同步器.北京航天航空大学学报.1994, 20(1) :25~30
[13]文乔,USB 接口虚拟示波器的研究与设计.武汉大学硕士学位论文,2005.
[14]华成英,童诗白.模拟电子技术基础(第四版).北京:高等教育出版社,2006:513-534.
[15]余祖俊等.基于USB的通用信号采集分析系统.电子测量与仪器学报.2005,1(019):85-89
[16]李贵山.印制电路板设计中的抗干扰措施与电磁兼容性研究.电子工艺技术.第 26卷,第 6 期,2001:248-251.
[17]赵晶.电路设计与制版 Protel 99 高级应用.北京人民邮电出版社,2000:50-151.
[18]王晗.PCB 设计中的注意事项.电子元器件.
[19]谢自美.电子线路设计、实验、测试.华中理工大学出版社,1992:18-35.
[20]刘治国.USB-1149.1 边界扫描测试控制器的设计.电子科技大学硕士学位论文,2004.5:17-18
[21]张剑波,颜钢锋.基于 GPIF 的 USB-ATA 解决方案.电子技术应用.2002.Vol.28.No.7.pp 14-17
[22]Savides,Tony; Dwolatzky,Barry. Radar Simulation Using the Shooting and Bouncing Ray Technique. Canadian Conference on Electrical and Computer Engineering v1 2003. Page(s): 307-310
[23]Rongfeng Ren ,hengchun tian ect, the anti-jamming measures of reading and writing signals in the paralleltransmission, ISTM/2001 4th International Symposium on Test and Measurement,Volume 1,2001.
[24]Larry Rollingson, Dean Dieble, “Warhead impact telemetry system” Recover system instrumentation branch of Naval weapons center.
[25]路宏年等.信号与测试系统.北京:国防工业出版社,1991:81-97.
[26]毕海,李永新.遥测脉码调制 PCM 编码的逻辑电路实现.电讯技术.2004,39(2): 44~46
[27]沈力,朱来文,陈宏伟等译.高速数字设计.电子工业出版社,2004.5:53-81.
[28]崔吉俊.火箭导弹测试技术.国防工业出版社,1999:32-68.
[29]段静辉.基于存储测试技术的炮射导弹测试系统的研究.华北工学院硕士学位论文,2000.
[30]Bruce Kaufman,On the use of COTS VME-based hardware to implement high performance recce solid state recorders,SPIE Vol.2803 1996.
[31]李东红.侵彻加速度存储测试系统的研究及其信号处理与分析.中北大学硕士学位论文,2004.
[32]张国雄,金篆芷.测控电路.2002.7:28-30.
[33]朱明武,李永新.动态测量原理.北京理工大学出版社,1993:67-96.
[34]Dennis L Feucht.Why Circuits Oscillate Spuriously,Part 2:Amplifier Loading.
[35]XILINX Corporation. Spartan23 FPGA family complete data sheet [Z].
[36]Digital Control Modules Databook, Intel Corporation, 1988.
[37]巫锴,基于 USB 接口的图像采集系统设计.重庆大学硕士学位论文,2005.5:55-57
[38]EZ-USB FX2 Technical Manual. www.usb.org
[39]阎石.数字电子技术基础.高等教育出版社,2006,5.
[40]Burnette, Randal; Myer, Robert.Multi-emitter radar simulation. Microwave Engineering European JUNE/JULY June/July 2003, Page(s): 21-24
[41]马丽.机载雷达视频回波的仿真与模拟,电子科技大学学位论文,2005:14-17.
[42]谢占魁,张文栋,申湘南.存储测试技术.测试技术学报,Vol.8,No.2,1994:25-31.
[43]许志宏,李鸿飞,李树剩.飞航导弹测试技术发展方向分析.海军航空工程学院学报.2001,第 16 卷.第 2 期.
[44]冯涛.可编程逻辑器件技术—MAX+PLUS II 入门与提高.2002:10.
[45]张训诰,肖德辉.可靠性及其应用.北京:兵器工业出版社,1991:89.
[46]阎敬业.星载三维成像雷达高度计系统设计与误差分析.北京:中国科学院空间科学与应用研究中心,2005:46-66.
[2]Seakr Engineering Inc.s Products Specifications, www.seakr.com
[3]Calculex Inc.s Products Specifications,www.calculex.com
[4]Bruce Kaufman.A NonvolatileSolid-State Recorder for 100,000g.Environments. Sensors Magazine .Vol. 17, No. 6, June 2005, 46-51.
[5]Bruce Kaufman,On the use of COTS VME-based hardware to implement high performance recce solid state recorders,Proceedings of SPIE - The International Society for Optical Engineering,2006:155～160.
[6]Howard Johnson、Martin Graham,High-Speed Digital Design,Publishing House of Electronics Industry,2003:25～29.
[7]李开明.航天高密度大容量数据存储技术的发展.电子技术应。第 25卷,第4期,2000:45-48.
[8]史彦斌等.航空电子综合测试系统的发展现状及趋势.计量技术.第 29 卷,第 4 期,2004:75-80.
[9]王小东,郝志航.大容量固态存储技术.光学精密工程.第9 卷.第4 期,2001:396-400.
[10]Flash Databook, Samsung Corporation, 2007.
[11]李宁.数字合成信号源及高速数据采集测试平台的研究. 成都:国防工业出版社, 2004:21-36.
[12]张军,姚远,张其善.高速可编程 PCM 遥测帧同步器.北京航天航空大学学报.1994, 20(1) :25~30
[13]文乔,USB 接口虚拟示波器的研究与设计.武汉大学硕士学位论文,2005.
[14]华成英,童诗白.模拟电子技术基础(第四版).北京:高等教育出版社,2006:513-534.
[15]余祖俊等.基于USB的通用信号采集分析系统.电子测量与仪器学报.2005,1(019):85-89
[16]李贵山.印制电路板设计中的抗干扰措施与电磁兼容性研究.电子工艺技术.第 26卷,第 6 期,2001:248-251.
[17]赵晶.电路设计与制版 Protel 99 高级应用.北京人民邮电出版社,2000:50-151.
[18]王晗.PCB 设计中的注意事项.电子元器件.
[19]谢自美.电子线路设计、实验、测试.华中理工大学出版社,1992:18-35.
[20]刘治国.USB-1149.1 边界扫描测试控制器的设计.电子科技大学硕士学位论文,2004.5:17-18
[21]张剑波,颜钢锋.基于 GPIF 的 USB-ATA 解决方案.电子技术应用.2002.Vol.28.No.7.pp 14-17
[22]Savides,Tony; Dwolatzky,Barry. Radar Simulation Using the Shooting and Bouncing Ray Technique. Canadian Conference on Electrical and Computer Engineering v1 2003. Page(s): 307-310
[23]Rongfeng Ren ,hengchun tian ect, the anti-jamming measures of reading and writing signals in the paralleltransmission, ISTM/2001 4th International Symposium on Test and Measurement,Volume 1,2001.
[24]Larry Rollingson, Dean Dieble, “Warhead impact telemetry system” Recover system instrumentation branch of Naval weapons center.
[25]路宏年等.信号与测试系统.北京:国防工业出版社,1991:81-97.
[26]毕海,李永新.遥测脉码调制 PCM 编码的逻辑电路实现.电讯技术.2004,39(2): 44~46
[27]沈力,朱来文,陈宏伟等译.高速数字设计.电子工业出版社,2004.5:53-81.
[28]崔吉俊.火箭导弹测试技术.国防工业出版社,1999:32-68.
[29]段静辉.基于存储测试技术的炮射导弹测试系统的研究.华北工学院硕士学位论文,2000.
[30]Bruce Kaufman,On the use of COTS VME-based hardware to implement high performance recce solid state recorders,SPIE Vol.2803 1996.
[31]李东红.侵彻加速度存储测试系统的研究及其信号处理与分析.中北大学硕士学位论文,2004.
[32]张国雄,金篆芷.测控电路.2002.7:28-30.
[33]朱明武,李永新.动态测量原理.北京理工大学出版社,1993:67-96.
[34]Dennis L Feucht.Why Circuits Oscillate Spuriously,Part 2:Amplifier Loading.
[35]XILINX Corporation. Spartan23 FPGA family complete data sheet [Z].
[36]Digital Control Modules Databook, Intel Corporation, 1988.
[37]巫锴,基于 USB 接口的图像采集系统设计.重庆大学硕士学位论文,2005.5:55-57
[38]EZ-USB FX2 Technical Manual. www.usb.org
[39]阎石.数字电子技术基础.高等教育出版社,2006,5.
[40]Burnette, Randal; Myer, Robert.Multi-emitter radar simulation. Microwave Engineering European JUNE/JULY June/July 2003, Page(s): 21-24
[41]马丽.机载雷达视频回波的仿真与模拟,电子科技大学学位论文,2005:14-17.
[42]谢占魁,张文栋,申湘南.存储测试技术.测试技术学报,Vol.8,No.2,1994:25-31.
[43]许志宏,李鸿飞,李树剩.飞航导弹测试技术发展方向分析.海军航空工程学院学报.2001,第 16 卷.第 2 期.
[44]冯涛.可编程逻辑器件技术—MAX+PLUS II 入门与提高.2002:10.
[45]张训诰,肖德辉.可靠性及其应用.北京:兵器工业出版社,1991:89.
[46]阎敬业.星载三维成像雷达高度计系统设计与误差分析.北京:中国科学院空间科学与应用研究中心,2005:46-66.