[go: up one dir, main page]

CN101604142A - Time information detection method of output signal of satellite synchronous timing device - Google Patents

Time information detection method of output signal of satellite synchronous timing device Download PDF

Info

Publication number
CN101604142A
CN101604142A CN 200810047989 CN200810047989A CN101604142A CN 101604142 A CN101604142 A CN 101604142A CN 200810047989 CN200810047989 CN 200810047989 CN 200810047989 A CN200810047989 A CN 200810047989A CN 101604142 A CN101604142 A CN 101604142A
Authority
CN
China
Prior art keywords
time
satellite
information
signal source
message
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN 200810047989
Other languages
Chinese (zh)
Other versions
CN101604142B (en
Inventor
陈宏�
潘杨
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
State Grid Corp of China SGCC
Electric Power Research Institute of State Grid Hubei Electric Power Co Ltd
Original Assignee
HUBEI PROV POWER TEST INST
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by HUBEI PROV POWER TEST INST filed Critical HUBEI PROV POWER TEST INST
Priority to CN 200810047989 priority Critical patent/CN101604142B/en
Publication of CN101604142A publication Critical patent/CN101604142A/en
Application granted granted Critical
Publication of CN101604142B publication Critical patent/CN101604142B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Electric Clocks (AREA)
  • Synchronisation In Digital Transmission Systems (AREA)

Abstract

一种卫星同步授时装置输出信号的时间信息检测方法,设定可控时标信号源(1)的脉冲信号输出端(4)的输出开放时间T,并置为到时触发方式,配合可控时标信号源(1)在指定T时刻(27)输出与卫星同步的脉冲起始1pps,触发示波器(2)捕捉卫星同步授时装置(3)的输出信号,完成卫星同步授时装置串行报文时间信息检测和卫星同步授时装置B码时间信息正确性的检测。该方法是一种可以更全面地测试电网子站卫星同步授时装置技术性能的检测方法,从而能够更完善地保障二次设备的时间同步准确性。

Figure 200810047989

A method for detecting time information of the output signal of a satellite synchronous timing device, setting the output opening time T of the pulse signal output terminal (4) of the controllable time scale signal source (1), and setting it as an arrival trigger mode, cooperating with the controllable time scale signal source (1) The time scale signal source (1) outputs the pulse start 1pps synchronous with the satellite at the specified time T (27), triggers the oscilloscope (2) to capture the output signal of the satellite synchronous timing device (3), and completes the serial message of the satellite synchronous timing device Time information detection and correctness detection of B code time information of satellite synchronous time service device. This method is a detection method that can more comprehensively test the technical performance of the satellite synchronous timing device of the substation of the power grid, so that the time synchronization accuracy of the secondary equipment can be more completely guaranteed.

Figure 200810047989

Description

卫星同步授时装置输出信号的时间信息检测方法 Time information detection method of output signal of satellite synchronous timing device

技术领域 technical field

本发明涉及电力设备测试方法,具体说是一种采用卫星信号用于电力设备时间同步的卫星同步授时装置输出信号的时间信息检测方法。The invention relates to a method for testing electric equipment, in particular to a method for detecting time information of an output signal of a satellite synchronous timing device using satellite signals for time synchronization of electric equipment.

背景技术 Background technique

电网对子站(含变电站、发电厂)自动化系统远动及其他相关电气二次智能电子设备(IED)时间同步性能,要求达到毫秒及以上的精度。二次设备时间同步性能,直接关系到电网子站内(本地)、子站间(异地)运行操作的正确性,以及对事故及时的准确分析和判断处理。The time synchronization performance of the grid's substation (including substations, power plants) automation system telecontrol and other related electrical secondary intelligent electronic devices (IEDs) requires an accuracy of milliseconds and above. The time synchronization performance of secondary equipment is directly related to the correctness of the operation within the sub-station (local) and between sub-stations (off-site), as well as the timely and accurate analysis and judgment of accidents.

卫星异地时间同步方式技术先进成熟、不受气候影响、不占用电力信道,在电网子站应用广泛。变电站多以卫星授时装置作为主选时钟源,对站内二次设备进行授时,保障各设备的时间同步。目前卫星授时装置,大都采用GPS卫星信号为授时装置本身的时间同步源,现场称其为GPS授时装置。The satellite off-site time synchronization method is advanced and mature in technology, not affected by climate, and does not occupy power channels, so it is widely used in power grid substations. Most substations use satellite timing devices as the main clock source to perform timing for secondary equipment in the station to ensure time synchronization of each equipment. At present, most satellite time service devices use GPS satellite signals as the time synchronization source of the time service device itself, and are called GPS time service devices on site.

变电站常用的卫星信号同步授时装置输出信号有三种类型:There are three types of output signals of satellite signal synchronous timing devices commonly used in substations:

校时脉冲输出:原理上与卫星时间基准脉冲信号同步,按每秒、每分或每小时节拍输出对时脉冲信号(PPS、PPM、PPH)。该信号为对时基准信号,不携带时间信息,通常与串行报文输出信号共同对设备授时。本类型包括静态空接点输出方式,授时装置按照校时脉冲的动作节拍控制接点的动作,两端施加外部电压作为校时脉冲的现场扩展应用。Timing pulse output: In principle, it is synchronized with the satellite time reference pulse signal, and outputs the timing pulse signal (PPS, PPM, PPH) at the beat of each second, minute or hour. This signal is a time synchronization reference signal, which does not carry time information, and is usually used together with the serial message output signal to provide time service to the device. This type includes static empty contact output mode, the timing device controls the action of the contact according to the action beat of the timing pulse, and the external voltage is applied at both ends as the field expansion application of the timing pulse.

串行报文输出:通常采用物理层遵循RS232、485、422标准的异步传输方式,或者采用以太网的物理层标准,传输的时间信息数据格式无统一要求。该类信号的时间基准精度较难保障。Serial message output: Usually, the physical layer follows the RS232, 485, 422 standard asynchronous transmission mode, or the physical layer standard of Ethernet, and there is no unified requirement for the data format of the time information transmitted. The time reference accuracy of this type of signal is difficult to guarantee.

B码输出:即遵循IRIG系列的B标准所规定的时间编码信息传输方式。通常由专用的调制解调部件实现,有直流脉宽调制和交流调幅等两种信息传递物理方式,每秒传递一帧信息(包含100个码元)、每帧信息占用一秒、每帧信息的起始对准卫星对时脉冲1pps上升沿、时间信息指向帧起始时刻。即,B码既有对时基准,也携带了对时基准的时间信息。B code output: It follows the time code information transmission method stipulated in the B standard of the IRIG series. It is usually realized by a dedicated modulation and demodulation component. There are two physical methods of information transmission, such as DC pulse width modulation and AC amplitude modulation. One frame of information (including 100 symbols) is transmitted per second, and each frame of information takes up one second. Each frame of information The starting point of the satellite is aligned with the rising edge of the 1pps pulse, and the time information points to the frame start time. That is, the B code not only has a time reference, but also carries the time information of the time reference.

卫星同步授时装置输出信号是被授时设备的时钟源,传统测试方式不易对其发送和携带的时间信息进行定时的有效捕获,无法完全达到时间正确性认定的目的。传统测试方法实际是对授时装置输出信号进行时间频率的偏差测试。卫星同步标准钟端口输出的脉冲信号是一个已经与卫星时间脉冲同步、不带有时间信息的节拍信号(或者,为一对时基准信号)。该方式由于不易确定所捕获时间信息的绝对时刻,因而不易确认秒脉冲信号对应的B码时间信息正确性,也不易检测串行报文的时间信息。The output signal of the satellite synchronous timing device is the clock source of the timed equipment. The traditional test method is not easy to effectively capture the time information sent and carried by it, and cannot fully achieve the purpose of determining the correctness of the time. The traditional test method is actually to test the time-frequency deviation of the output signal of the timing device. The pulse signal output by the satellite synchronous standard clock port is a beat signal (or a pair of time reference signals) that has been synchronized with the satellite time pulse and does not contain time information. Since it is difficult to determine the absolute time of the captured time information in this method, it is difficult to confirm the correctness of the B-code time information corresponding to the second pulse signal, and it is also difficult to detect the time information of the serial message.

由于可控时标信号源装置(另案申请)的出现,使得标准时钟源的输出冲脉可以控制在指定时间输出,输出的时钟脉冲信号成为已知某个确定时刻的输出脉冲,同时可控时标信号源带有由确定精度高于毫秒级的时间控制的开关,从而能够确定卫星同步授时装置的输出信息。Due to the appearance of the controllable time scale signal source device (another application), the output pulse of the standard clock source can be controlled to be output at a specified time, and the output clock pulse signal becomes an output pulse at a known certain time. The marker signal source has a switch controlled by the time with a determination accuracy higher than millisecond level, so that the output information of the satellite synchronous timing device can be determined.

发明内容 Contents of the invention

本发明的目的是提供一种可以更全面地检测时钟源设备技术性能,从而保障子站二次设备时间同步准确性的一种卫星同步授时装置输出信号的时间信息检测方法。The purpose of the present invention is to provide a time information detection method of the output signal of a satellite synchronous timing device that can more comprehensively detect the technical performance of the clock source equipment, thereby ensuring the time synchronization accuracy of the secondary equipment of the substation.

所述卫星同步授时装置输出信号的时间信息检测方法中,卫星同步授时装置串行报文时间信息检测方法,用到以下设备:卫星同步授时装置、多通道存储示波器、可控时标信号源、通信转换器、计算机。In the time information detection method of the output signal of the satellite synchronous timing device, the satellite synchronous timing device serial message time information detection method uses the following equipment: satellite synchronous timing device, multi-channel storage oscilloscope, controllable time scale signal source, Communication converters, computers.

可控时标信号源的脉冲信号输出端,接入示波器的检测通道A;卫星同步授时装置的串行报文输出端,接入示波器的检测通道B;卫星天线一和卫星天线二,分别连接至卫星同步授时装置的接收端和可控时标信号源的接收端;卫星同步授时装置的串行报文输出端X1,连接至可控时标信号源上控制开关S的无源接点S1端;卫星同步授时装置的串行报文输出端X2,连接至通信转换器输入端C2;可控时标信号源上控制开关S的无源接点S2端,连接至通信转换器输入端C1;通信转换器的输出端连接至计算机的通信接口。The pulse signal output terminal of the controllable time scale signal source is connected to the detection channel A of the oscilloscope; the serial message output terminal of the satellite synchronous timing device is connected to the detection channel B of the oscilloscope; satellite antenna one and satellite antenna two are respectively connected to To the receiving end of the satellite synchronous timing device and the receiving end of the controllable time scale signal source; the serial message output terminal X1 of the satellite synchronous time service device is connected to the passive contact S1 end of the control switch S on the controllable time scale signal source ; The serial message output terminal X2 of the satellite synchronous timing device is connected to the input terminal C2 of the communication converter; the passive contact S2 end of the control switch S on the controllable time scale signal source is connected to the input terminal C1 of the communication converter; The output end of the converter is connected to the communication interface of the computer.

所测试的报文时间信息为“T时间报文”信息,其特征是:“T时间报文”信息经过以下步骤从计算机采集到:The tested message time information is "T time message" information, which is characterized in that: "T time message" information is collected from the computer through the following steps:

①、可控时标信号源的控制开关S闭合,计算机处于正常接收卫星同步授时装置的串行报文输出端X所输出的报文信息状态;①. The control switch S of the controllable time scale signal source is closed, and the computer is in the state of normally receiving the message information output by the serial message output terminal X of the satellite synchronous timing device;

②、设定可控时标信号源的脉冲信号输出端的输出开放时间T,并置为到时触发方式,设定可控时标信号源的控制开关S断开时刻为指定T时刻+控制开关S的动作起始延迟时间ΔT时刻;②. Set the output opening time T of the pulse signal output terminal of the controllable time scale signal source, and set it as the time-out trigger mode, and set the time when the control switch S of the controllable time scale signal source is turned off is the specified T time + control switch The action start delay time ΔT moment of S;

③、可控时标信号源在指定T时刻输出T时刻卫星同步脉冲起始的1pps;③. The controllable time scale signal source outputs 1pps at the beginning of the satellite synchronization pulse at time T at the specified time T;

④、在指定T时刻+控制开关S的动作起始延迟时间ΔT时刻,断开可控时标信号源的控制开关S,计算机最终接收到指定T时刻后的第一个串行报文数据帧即“T时间报文”信息,以及指定T时刻前的最后数据帧即“T-1sec时间报文”信息。④. At the specified time T + the action start delay time ΔT of the control switch S, turn off the control switch S of the controllable time scale signal source, and the computer finally receives the first serial message data frame after the specified T time That is, the "T time message" information, and the last data frame before the specified time T, that is, the "T-1sec time message" information.

所述示波器与可控时标信号源的测试准备状态为:示波器的通道A设为脉冲输入信号上升沿触发显示方式,可控时标信号源和卫星同步授时装置均与卫星同步,可控时标信号源的控制开关S的无源接点两端闭合。The test preparation state of the oscilloscope and the controllable time scale signal source is: the channel A of the oscilloscope is set as the rising edge trigger display mode of the pulse input signal, the controllable time scale signal source and the satellite synchronous timing device are all synchronized with the satellite, and the controllable time scale The two ends of the passive contact of the control switch S marked with the signal source are closed.

可控时标信号源在指定T时刻输出T时刻的卫星同步脉冲起始的1pps,示波器的通道A、B捕获到“T时间报文”信息波形,并由此测得T时刻到“T时间报文”信息起始时刻的时间Δt1,以及“T时间报文”信息起、止所需时间Δt。The controllable time scale signal source outputs 1pps at the beginning of the satellite synchronization pulse at the time T at the specified time T, and the channels A and B of the oscilloscope capture the information waveform of the "T time message", and thus measure the time from T time to "T time The time Δt1 of the starting moment of the "T time message" information, and the time Δt required for the start and end of the "T time message" information.

所述控制开关S的动作起始延迟时间ΔT为(T时刻到“T时间报文”信息起始时刻的时间Δt1+T时间报文信息起、止所需时间Δt)由示波器根据通道A接收的指定T时刻信号的上升沿随机测出,在采集“T时间报文”信息之前预先得到。The action start delay time ΔT of the control switch S is (the time Δt1 from the time T to the start time of the "T time message" information + the time Δt required for the start and end of the T time message information) to be received by the oscilloscope according to channel A The rising edge of the signal at the specified time T is randomly measured and obtained in advance before collecting the "T time message" information.

所述延迟时间ΔT在如下时间范围内:(T时刻到“T时间报文”信息起始时刻的时间Δt1+“T时间报文”信息起、止所需时间Δt)<ΔT<1秒。The delay time ΔT is within the following time range: (time Δt1 from time T to the start time of the "T time message" information + time Δt required for the start and end of the "T time message" information)<ΔT<1 second.

所述可控时标信号源在指定T时刻发出的脉冲信号可以是单脉冲,也可以是频率脉冲信号。The pulse signal sent by the controllable time scale signal source at the specified time T may be a single pulse or a frequency pulse signal.

卫星同步授时装置输出信号的时间信息检测方法中,卫星同步授时装置B码时间信息正确性的检测方法,用到以下设备:卫星同步授时装置、多通道存储示波器、可控时标信号源。In the time information detection method of the output signal of the satellite synchronous timing device, the detection method of the correctness of the B code time information of the satellite synchronous timing device uses the following equipment: a satellite synchronous timing device, a multi-channel storage oscilloscope, and a controllable time scale signal source.

可控时标信号源的脉冲信号输出端,接入示波器的检测通道A;卫星同步授时装置的B码信号输出端,接入示波器的检测通道C;卫星天线一和卫星天线二,分别连接至卫星同步授时装置的接收端和可控时标信号源的接收端。The pulse signal output terminal of the controllable time scale signal source is connected to the detection channel A of the oscilloscope; the B code signal output terminal of the satellite synchronous timing device is connected to the detection channel C of the oscilloscope; satellite antenna 1 and satellite antenna 2 are respectively connected to The receiving end of the satellite synchronous timing device and the receiving end of the controllable time scale signal source.

所测试的B码时间信息为“T时间IRIG-B编码波形”时间信息,其特征是:“T时间IRIG-B编码波形”时间信息由以下步骤检验:The tested B code time information is "T time IRIG-B encoded waveform" time information, which is characterized in that the "T time IRIG-B encoded waveform" time information is checked by the following steps:

①、关闭可控时标信号源的脉冲信号输出端的输出,示波器设置通道A为脉冲输入信号上升沿触发显示方式;①. Turn off the output of the pulse signal output terminal of the controllable time scale signal source, and set the channel A of the oscilloscope to the rising edge trigger display mode of the pulse input signal;

②、设定可控时标信号源的脉冲信号输出端输出开放时间T并置为到时触发方式;②. Set the pulse signal output terminal of the controllable time scale signal source to output the opening time T and set it as the time-out trigger mode;

③、可控时标信号源的脉冲信号输出端输出指定T时刻的卫星同步脉冲起始的1pps,通过示波器的通道A、C捕获到“T时间的IRIG-B编码波形”;③. The pulse signal output terminal of the controllable time scale signal source outputs 1pps at the beginning of the satellite synchronization pulse at the specified time T, and the "IRIG-B coded waveform at T time" is captured through channels A and C of the oscilloscope;

④、根据“T时间IRIG-B编码波形”读出时间信息,比较其与可控时标信号源所设定时间T的一致性。④. Read the time information according to the "T time IRIG-B code waveform", and compare its consistency with the time T set by the controllable time scale signal source.

可控时标信号源在指定T时刻发出的脉冲信号可以是单脉冲信号,也可以是频率脉冲信号。The pulse signal sent by the controllable time scale signal source at the specified time T can be a single pulse signal or a frequency pulse signal.

本发明涵盖了传统的测试内容,能够可控的获取卫星同步授时装置输出的信号和信息,在指定的测试时刻检测卫星同步授时装置输出端口发送信号的准确性和信息正确性,可以全面的检测时钟源设备的技术性能,从而保障子站二次设备时间同步的准确性,可以为子站自动化系统和二次设备的验收、改造、改进等提供技术依据,有利于电网安全生产和稳定运行。The invention covers the traditional test content, can controllably obtain the signal and information output by the satellite synchronous timing device, and detect the accuracy of the signal sent by the output port of the satellite synchronous timing device and the correctness of information at the specified test time, and can comprehensively detect The technical performance of the clock source equipment, so as to ensure the accuracy of time synchronization of the secondary equipment of the substation, can provide technical basis for the acceptance, transformation and improvement of the automation system and secondary equipment of the substation, and is conducive to the safe production and stable operation of the power grid.

附图说明 Description of drawings

图1是传统测试方法设备连接示意图,Figure 1 is a schematic diagram of the traditional test method equipment connection,

图2是传统测试方法波形示意图,Figure 2 is a schematic diagram of the traditional test method waveform,

图3是传统测试流程图,Figure 3 is a traditional test flow chart,

图4是本发明设备连接示意图,Fig. 4 is a schematic diagram of device connection of the present invention,

图5是本发明测试方法信号时序图,Fig. 5 is a signal timing diagram of the test method of the present invention,

图6是本发明B码测试流程图,Fig. 6 is the flow chart of B code test of the present invention,

图7是本发明串行报文测试流程图。Fig. 7 is a flow chart of the serial message test of the present invention.

图中:1-可控时标信号源,2-示波器,3-卫星同步授时装置,4-脉冲信号输出端,5-可控时标信号源的控制开关S,6-通信转换器,7-通信转换器的输出端,8-计算机的通信接口,9-计算机,10-卫星同步授时装置的校时脉冲输出端Z,11-卫星同步授时装置的B码输出端Y,12-卫星同步授时装置的串行报文输出端X1,13-卫星同步授时装置的串行报文输出端X2,14-控制开关S的无源接点S1端,15-控制开关S的无源接点S2端,16-通信转换器输入端C1,17-通信转换器输入端C2,18-卫星天线一,19-卫星天线二,20-可控时标信号源控制开关动作波形,21-可控时标信号源脉冲输出端波形,22-卫星同步授时装置报文输出端X波形,23-卫星同步授时装置B码输出端Y波形,24-卫星同步授时装置较时脉冲输出端Z波形,25-控制开关S的动作起始延迟时间ΔT,26-计算机报文接收中断时刻,27-指定T时刻,28-T时刻到“T时间报文”信息起始时刻的时间Δt1,29-T时间报文信息起、止所需时间Δt,30-T时刻到T时间B码输出起始时刻的时间Δt2,31-T时刻到T时间较时脉冲输出起始时刻的时间Δt3,32-“T时间报文”信息波形,33-T时间IRIG-B编码波形,34-第-步,35-第二步,36-第三步,37-第四步,38-第五步,39-B码测试第-步,40-B码测试第二步,41-B码测试第三步,42-B码测试第四步,43-串行报文测试第一步,44-串行报文测试第二步,45-串行报文测试第三步,46-串行报文测试第四步,47-串行报文测试第五步,48-串行报文测试第六步,49-卫星同步标准钟,50-“T-1sec时间报文”信息波形。In the figure: 1-controllable time scale signal source, 2-oscilloscope, 3-satellite synchronous timing device, 4-pulse signal output terminal, 5-control switch S of controllable time scale signal source, 6-communication converter, 7 -The output terminal of the communication converter, 8-the communication interface of the computer, 9-the computer, 10-the timing pulse output terminal Z of the satellite synchronous timing device, 11-the B code output terminal Y of the satellite synchronous timing device, 12-the satellite synchronous Serial message output terminal X1 of the time service device, 13-serial message output terminal X2 of the satellite synchronous time service device, 14-the passive contact S1 terminal of the control switch S, 15-the passive contact S2 terminal of the control switch S, 16-communication converter input terminal C1, 17-communication converter input terminal C2, 18-satellite antenna 1, 19-satellite antenna 2, 20-controllable time scale signal source control switch action waveform, 21-controllable time scale signal Waveform of source pulse output terminal, 22-X waveform of message output terminal of satellite synchronous time service device, 23-Y waveform of B code output terminal of satellite synchronous time service device, 24-Z waveform of time pulse output terminal of satellite synchronous time service device, 25-control switch S’s action start delay time ΔT, 26-computer message receiving interruption time, 27-designated T time, 28-T time to the time Δt1 of the "T time message" information start time, 29-T time message information The time required for start and stop Δt, the time Δt2 from 30-T time to T time B code output start time, the time 31-T time to T time pulse output start time Δt3, 32-"T time message "Information waveform, 33-T time IRIG-B code waveform, 34-step-step, 35-step 2, 36-step 3, 37-step 4, 38-step 5, 39-B code test step -step, 40-B code test second step, 41-B code test third step, 42-B code test fourth step, 43-serial message test first step, 44-serial message test second Step, 45-serial message test step 3, 46-serial message test step 4, 47-serial message test step 5, 48-serial message test step 6, 49-satellite synchronization Standard clock, 50-"T-1sec time message" information waveform.

具体实施方式 Detailed ways

下面结合附图对发明进一步说明:Below in conjunction with accompanying drawing, invention is further described:

作为对比,以下简要介绍一下传统的卫星同步授时装置测试方法,如图1中所示为传统的卫星同步授时装置测试装置及连接图。As a comparison, the following briefly introduces the traditional satellite synchronous timing device test method, as shown in Figure 1 is the traditional satellite synchronous timing device test device and connection diagram.

在图1中,卫星同步标准钟49输出的脉冲信号P_1pps,既可以与卫星时间同步也可以由内部标准源提供;卫星同步标准钟49和示波器2组成测试设备;卫星同步授时装置3为被测试设备。图2为传统测试方法下的示波器波形示意图。In Fig. 1, the pulse signal P_1pps of satellite synchronous standard clock 49 output, both can be with satellite time synchronization also can be provided by internal standard source; Satellite synchronous standard clock 49 and oscilloscope 2 form test equipment; Satellite synchronous time service device 3 is tested equipment. Figure 2 is a schematic diagram of an oscilloscope waveform under a traditional test method.

图1中,卫星同步标准钟49的脉冲信号输出端4输出的脉冲信号接入示波器2的检测通道A;卫星同步授时装置3的串行报文输出端12、13,接入示波器的检测通道B;每秒一帧的IRIG-B标准信号B码输出端11、校时脉冲输出端10,分别接入示波器的检测通道C、D;图1中的卫星天线一18和卫星天线二19,分别连接至卫星同步授时装置接收端和卫星同步标准钟接收端。Among Fig. 1, the pulse signal output of the pulse signal output end 4 of the satellite synchronous standard clock 49 is connected to the detection channel A of the oscilloscope 2; the serial message output terminals 12, 13 of the satellite synchronous timing device 3 are connected to the detection channel of the oscilloscope B; the IRIG-B standard signal B code output terminal 11 and the timing pulse output terminal 10 of one frame per second are connected to the detection channels C and D of the oscilloscope respectively; satellite antenna one 18 and satellite antenna two 19 in Fig. 1, Connect to the receiving end of the satellite synchronous timing device and the receiving end of the satellite synchronous standard clock respectively.

图3为传统测试方法的测试流程框图,以卫星同步授时装置3和卫星同步标准钟49均每秒发送一次信号为例,图1、图2和图3所表示测试方法的步骤如下:Fig. 3 is the test flow block diagram of traditional test method, with the satellite synchronous timing device 3 and the satellite synchronous standard clock 49 all sending a signal per second as an example, the steps of the test method shown in Fig. 1, Fig. 2 and Fig. 3 are as follows:

如图3所示,第一步34:在图1中,保证卫星同步授时装置3与卫星同步正常、卫星同步标准钟49输出P_1pps与卫星脉冲信号同步;As shown in Figure 3, the first step 34: in Figure 1, guarantee that satellite synchronous timing device 3 is normal with satellite synchronization, satellite synchronous standard clock 49 outputs P_1pps and satellite pulse signal synchronization;

第二步35:以卫星同步标准钟49的脉冲信号输出端4发送的秒脉冲节拍信号P_1pps作为对时基准,可随机测出示波器2的通道A分别与示波器2的通道B、C、D之间的差值,即图2的Δt1、Δt2、Δt3;Second step 35: the second pulse beat signal P_1pps sent by the pulse signal output terminal 4 of the satellite synchronous standard clock 49 is used as the time reference, and the channel A of the oscilloscope 2 and the channel B, C, D of the oscilloscope 2 can be measured at random. The difference between, that is, Δt1, Δt2, Δt3 in Figure 2;

第三步36:如需测试图1中卫星同步授时装置3内部守时状态的输出信号X、Y、Z稳定性,则进行第四步37,否则测试结束;The third step 36: if the output signal X, Y, Z stability of the internal punctuality state of the satellite synchronous timing device 3 in the test Fig. 1 is needed, then carry out the fourth step 37, otherwise the test ends;

第四步37:在图1中,断开卫星同步授时装置3的卫星天线一18,卫星同步授时装置3将依靠内部时钟的守时,保证输出端(X、Y、Z)12、13、11、10信号的持续;在图1中,断开卫星同步标准钟49的卫星天线二19,脉冲信号输出端4输出信号P_1pps脉冲的节拍将由卫星同步标准钟49的内部标准时钟源维持;The 4th step 37: in Fig. 1, disconnect the satellite antenna one 18 of satellite synchronous time service device 3, satellite synchronous time service device 3 will rely on the punctuality of internal clock, guarantee output terminal (X, Y, Z) 12,13, 11,10 signal continuity; In Fig. 1, disconnect the satellite antenna two 19 of satellite synchronous standard clock 49, the beat of pulse signal output terminal 4 output signal P_1pps pulse will be maintained by the internal standard clock source of satellite synchronous standard clock 49;

第五步38:仍以图1的卫星同步标准钟49信号输出端4的脉冲信号P_1pps为基准,每间隔一段时间按照第二步35的方法,重复测试图2的Δt1、Δt2、Δt3,得出卫星同步授时装置3内部守时状态下输出信号的稳定性;The fifth step 38: still take the pulse signal P_1pps of the signal output terminal 4 of the satellite synchronous standard clock 49 in Fig. 1 as a benchmark, repeat the test of Δt1, Δt2, and Δt3 in Fig. 2 according to the method of the second step 35 at intervals, and obtain Detect the stability of the output signal under the internal timing state of the satellite synchronous timing service device 3;

测试结束。The test is over.

传统测试方法实际是对卫星同步授时装置3输出信号进行时间频率的偏差测试。卫星同步标准钟49的脉冲信号输出端4输出的脉冲信号是一个已经与卫星时间脉冲同步、不带有时间信息的节拍信号(或者,为一对时基准信号)。该方式不易确认秒脉冲信号对应的B码时间信息正确性,也不易检测串行报文的时间信息。其原因是无法确定所捕获时间信息的绝对时间。The traditional test method is actually to test the time frequency deviation of the output signal of the satellite synchronous timing device 3 . The pulse signal output by the pulse signal output terminal 4 of the satellite synchronous standard clock 49 is a beat signal (or a pair of time reference signals) that has been synchronized with the satellite time pulse and does not have time information. This method is not easy to confirm the correctness of the B code time information corresponding to the second pulse signal, and it is not easy to detect the time information of the serial message. The reason for this is that the absolute time of the captured time information cannot be determined.

本发明测试方法涵盖传统测试,能够可控地捕获卫星同步授时装置输出信号的时间信息。The testing method of the invention covers traditional testing and can controllably capture the time information of the output signal of the satellite synchronous timing device.

图4即是本发明测试方法的设备构成和连接方式示意图。在图4中,由可控时标信号源1、示波器2、通信转换器6和计算机9组成的测试设备,测试卫星同步授时装置3的输出信号及其携带的时间信息。Fig. 4 is a schematic diagram of the equipment composition and connection mode of the testing method of the present invention. In Fig. 4, the test equipment composed of controllable time scale signal source 1, oscilloscope 2, communication converter 6 and computer 9 tests the output signal of satellite synchronous timing device 3 and the time information it carries.

本测试方法反映在图4中,用可控时标信号源1取代了传统测试方法图1中的卫星同步标准钟49;通信转换器6,可为不同标准的通信接口转换器,也可为计算机的通信接口8的外部连接器。This test method is reflected in Fig. 4, has replaced the satellite synchronous standard clock 49 in traditional test method Fig. 1 with controllable time scale signal source 1; Communication converter 6 can be the communication interface converter of different standards, also can be 8 external connectors for the computer's communication interface.

图4中,可控时标信号源1的特点如下:In Figure 4, the characteristics of the controllable time scale signal source 1 are as follows:

a、可控时标信号源1可在卫星实时同步方式下工作,也可在与卫星同步后,在内部标准时钟源守时的方式下工作;a. The controllable time scale signal source 1 can work in the mode of satellite real-time synchronization, and can also work in the mode of keeping time with the internal standard clock source after synchronizing with the satellite;

b、脉冲信号输出端4输出的脉冲节拍输出信号P_1pps,既可以为卫星同步脉冲,也可以从卫星同步转为内部标准源守时维持脉冲节拍;b. The pulse beat output signal P_1pps output by the pulse signal output terminal 4 can be a satellite synchronous pulse, or can be converted from satellite synchronization to an internal standard source to maintain the pulse beat on time;

c、可控时标信号源1可以在指定时刻由脉冲信号输出端4送出脉冲节拍P_1pps信号,也可以随时关闭脉冲信号输出端4的信号输出;c. The controllable time scale signal source 1 can send a pulse beat P_1pps signal from the pulse signal output terminal 4 at a specified time, and can also close the signal output of the pulse signal output terminal 4 at any time;

d、可控时标信号源1指定其控制开关S5的无源接点的通、断时刻。d. The controllable time scale signal source 1 designates the on-off time of the passive contact of the control switch S5.

图4中,本测试方法的设备连接方式:In Figure 4, the equipment connection mode of this test method:

可控时标信号源1的脉冲信号输出端4输出的P_1pps,接入示波器2的检测通道A;The P_1pps output by the pulse signal output terminal 4 of the controllable time scale signal source 1 is connected to the detection channel A of the oscilloscope 2;

卫星同步授时装置3的串行报文输出端12、13(X的X1和X2)、B码输出端11(Y的Y1和Y2)、校时脉冲输出端10(Z的Z1和Z2),分别接入示波器2的检测通道B、C、D;Serial message output 12,13 (X1 and X2 of X), B code output 11 (Y1 and Y2 of Y), timing pulse output 10 (Z1 and Z2 of Z) of satellite synchronous timing device 3, Connect to detection channels B, C, and D of oscilloscope 2 respectively;

卫星天线一18和卫星天线二19,分别连接至卫星同步授时装置3的接收端和可控时标信号源1的接收端。The first satellite antenna 18 and the second satellite antenna 19 are respectively connected to the receiving end of the satellite synchronous timing device 3 and the receiving end of the controllable time scale signal source 1 .

卫星同步授时装置3的串行报文输出端X1端12,连接至可控时标信号源1的控制开关无源接点S1端14;The serial message output terminal X1 terminal 12 of the satellite synchronous timing device 3 is connected to the control switch passive contact S1 terminal 14 of the controllable time scale signal source 1;

卫星同步授时装置3的串行报文输出端X2端13,连接至通信转换器6的输入端C2端17;The serial message output terminal X2 terminal 13 of the satellite synchronous timing device 3 is connected to the input terminal C2 terminal 17 of the communication converter 6;

可控时标信号源1的控制开关无源接点S2端15,连接至通信转换器6的输入端C1端16;The control switch passive contact S2 terminal 15 of the controllable time scale signal source 1 is connected to the input terminal C1 terminal 16 of the communication converter 6;

通信转换器6的输出端7,连接至计算机9的通信接口8。The output terminal 7 of the communication converter 6 is connected to the communication interface 8 of the computer 9 .

一、本测试方法对于传统测试项目的检测,完全可以参照前述图1、2、3描述的传统测试方法和步序进行。1. For the detection of traditional test items by this test method, it can be carried out with reference to the traditional test method and steps described in Figures 1, 2 and 3 above.

仍以卫星同步授时装置3和可控时标信号源1(不操作开关S)的输出均每秒发送一次信号为例,按照图4、2、3表述传统测试的步骤如下:Still taking the output of the satellite synchronous timing device 3 and the controllable time scale signal source 1 (without operating the switch S) to send a signal once per second as an example, the traditional test steps are described as follows according to Figures 4, 2, and 3:

按照图3第一步34:在图4中,保证卫星同步授时装置3与卫星同步正常、启动可控时标信号源1输出P_1pps与卫星脉冲信号同步;According to Fig. 3 first step 34: in Fig. 4, guarantee that satellite synchronous timing device 3 and satellite synchronization are normal, start controllable time scale signal source 1 output P_1pps and satellite pulse signal synchronization;

按照图3第二步35:图4中,以可控时标信号源1的脉冲信号输出端4发送的秒脉冲节拍信号P_1pps作为对时基准,可随机测出示波器2的通道A分别与示波器2的通道B、C、D之间的差值,即图2的Δt1、Δt2、Δt3;According to the second step 35 of Fig. 3: in Fig. 4, the pulse-per-second beat signal P_1pps sent by the pulse signal output terminal 4 of the controllable time scale signal source 1 is used as the time synchronization reference, and the channel A of the oscilloscope 2 can be randomly measured with the oscilloscope respectively. The difference between channels B, C, and D of 2, that is, Δt1, Δt2, and Δt3 in Figure 2;

按照图3第三步36:如需测试图4中卫星同步授时装置3内部授时状态的输出信号X、Y、Z稳定性,则进行第四步37,否则测试结束;According to the third step 36 of Fig. 3: as the output signal X, Y, Z stability of the internal timing state of the satellite synchronous timing device 3 in the test Fig. 4, then carry out the fourth step 37, otherwise the test ends;

按照图3第四步37:在图4中,断开卫星同步授时装置3的卫星天线一18,卫星同步授时装置3将依靠内部时钟的授时,保证卫星同步授时装置3输出端信号X、Y、Z的持续;在图4中,断开可控时标信号源1的卫星天线二19,脉冲信号输出端4输出信号P_1pps脉冲的节拍跟踪可控时标信号源1的内部标准时钟源;According to Fig. 3 fourth step 37: in Fig. 4, disconnect the satellite antenna one 18 of satellite synchronous time service device 3, satellite synchronous time service device 3 will rely on the time service of internal clock, guarantee that satellite synchronous time service device 3 output terminal signals X, Y , the continuity of Z; In Fig. 4, disconnect the satellite antenna two 19 of controllable time scale signal source 1, the internal standard clock source of the beat tracking controllable time scale signal source 1 of pulse signal output terminal 4 output signal P_1pps pulse;

按照图3第五步38:仍以图4可控时标信号源1的脉冲信号输出端4脉冲信号P_1pps为基准,每间隔一段时间按照第二步35的方法,重复测试图2的Δt1、Δt2、Δt3,得出卫星同步授时装置3内部授时状态下输出信号的稳定性;According to the fifth step 38 in Fig. 3: still taking the pulse signal P_1pps of the pulse signal output terminal 4 of the controllable time scale signal source 1 in Fig. 4 as a benchmark, repeat the test of Δt1, Δt2, Δt3, draw the stability of the output signal under the internal timing state of the satellite synchronous timing device 3;

测试结束。The test is over.

由于图4可控时标信号源1具有选择P_1pps输出某个指定时间卫星脉冲的功能,因此可以在某个时刻检测卫星同步授时装置3的信号输出误差,而不限于随机检测。即可以检测图5中指定T时刻27下的Δt1、Δt2、Δt3。Since the controllable time scale signal source 1 in FIG. 4 has the function of selecting P_1pps to output satellite pulses at a specified time, the signal output error of the satellite synchronous timing device 3 can be detected at a certain moment, and is not limited to random detection. That is, Δt1 , Δt2 , and Δt3 at the specified time T 27 in FIG. 5 can be detected.

二、B码时间信息检测2. B code time information detection

在图4中,可检测卫星同步授时装置3在指定时间下的“B码输出”信号Y携带的时间信息,图6为检测方法的流程,该项检测步骤如下:In Fig. 4, it is possible to detect the time information carried by the "B code output" signal Y of the satellite synchronous timing device 3 at a specified time, and Fig. 6 is the flow process of the detection method, and the detection steps are as follows:

图6的B码测试第一步39:图4中可控时标信号源1和卫星同步授时装置3均与卫星同步,图4中可控时标信号源1的脉冲信号输出端4输出信号与卫星的1pps脉冲同步、卫星同步授时装置3的“B码输出”端11(即Y的Y1和Y2)每秒发送一次信号,检查图4示波器2通道A、C的信号接收正常;The first step 39 of the B code test in Figure 6: the controllable time scale signal source 1 and the satellite synchronous timing device 3 are all synchronized with the satellite in Figure 4, and the pulse signal output terminal 4 of the controllable time scale signal source 1 outputs the signal in Figure 4 With the 1pps pulse synchronization of the satellite, the "B code output" terminal 11 (i.e. Y1 and Y2 of Y) of the satellite synchronous timing device 3 sends a signal once per second, check that the signal reception of the oscilloscope 2 channels A and C in Fig. 4 is normal;

图6的B码测试第二步40:如图4中,关闭可控时标信号源1的脉冲信号输出端4的输出,示波器2设置通道A为脉冲输入信号上升沿触发显示方式;The second step 40 of the B code test in Fig. 6: as shown in Fig. 4, close the output of the pulse signal output terminal 4 of the controllable time scale signal source 1, and the oscilloscope 2 sets channel A as the rising edge trigger display mode of the pulse input signal;

图6的B码测试第三步41:如图4中所示,设定可控时标信号源1的脉冲信号输出端4输出开放时间T并置为到时触发方式,T时刻为图5所示通道A期望捕捉的指定P_1pps信号在指定时刻的卫星同步脉冲上升沿;The third step 41 of the B code test in Fig. 6: as shown in Fig. 4, set the pulse signal output terminal 4 of the controllable time scale signal source 1 to output the opening time T and set it as the time-out trigger mode, and the time T is as Fig. 5 The rising edge of the satellite synchronization pulse at the specified time of the specified P_1pps signal that channel A expects to capture;

图6的B码测试第四步42:如图4中所示可控时标信号源1的脉冲信号输出端4,输出T时刻卫星同步脉冲起始的1pps,通过图4示波器2的通道A、C捕获到图5的指定T时刻27和图5的T时间“IRIG-B编码”波形33,可根据图5的T时间“IRIG-B编码”波形33读出时间信息,比较其与图4可控时标信号源1设定时间T的一致性;The fourth step 42 of the B code test in Fig. 6: the pulse signal output terminal 4 of the controllable time scale signal source 1 as shown in Fig. 4, output 1pps of the satellite synchronous pulse initiation at time T, and pass through the channel A of the oscilloscope 2 in Fig. 4 , C captures the specified T time 27 of Fig. 5 and the T time "IRIG-B code" waveform 33 of Fig. 5, the time information can be read out according to the T time "IRIG-B code" waveform 33 of Fig. 5, and compares it with that in Fig. 4 The consistency of the time T set by the controllable time scale signal source 1;

测试结束。The test is over.

三、串行报文时间信息检测3. Serial packet time information detection

在图4中可定时检测授时装置3串行报文输出端12、13(即X的X1和X2)发送的时间信息。图7为检测方法的流程,检测步骤如下:In FIG. 4 , the time information sent by the serial message output terminals 12 and 13 (that is, X1 and X2 of X) of the timing device 3 can be regularly detected. Fig. 7 is the flow process of detection method, and detection step is as follows:

图7的串行报文测试第一步43:如图4可控时标信号源1和卫星同步授时装置3均与卫星同步,图4可控时标信号源1的脉冲信号输出端4输出信号与卫星的1pps脉冲同步、可控时标信号源1的可控开关S5闭合、卫星同步授时装置3的串行报文输出端12、13(即X的X1和X2)每秒发送一次报文信号;The first step 43 of the serial message test in Figure 7: as shown in Figure 4, the controllable time scale signal source 1 and the satellite synchronous timing device 3 are all synchronized with the satellite, and the pulse signal output terminal 4 of the controllable time scale signal source 1 in Figure 4 outputs The signal is synchronized with the 1pps pulse of the satellite, the controllable switch S5 of the controllable time scale signal source 1 is closed, and the serial message output terminals 12 and 13 of the satellite synchronous timing device 3 (that is, X1 and X2 of X) send a report once per second Text signal;

图7的串行报文测试第二步44:图4中所示,检查示波器2通道A、B的信号接收正常,检查计算机9能够正常接收卫星同步授时装置3的X输出报文信息;The second step 44 of the serial message test of Fig. 7: as shown in Fig. 4, check that the signal reception of oscilloscope 2 channels A, B is normal, check that computer 9 can normally receive the X output message information of satellite synchronous timing device 3;

图7的串行报文测试第三步45:图4示波器2可以根据图5通道A接收信号的上升沿,随机测出图5通道B波形中的T时刻到“T时间报文”信息起始时刻的时间Δt128,以及测出图5“T时间报文”信息起、止所需时间29Δt,得到(Δt1+Δt);图4中关闭可控时标信号源1的脉冲信号输出端4的脉冲输出信号、示波器2设置通道A为脉冲输入信号上升沿触发显示方式;The third step 45 of the serial message test in Figure 7: the oscilloscope 2 in Figure 4 can randomly measure the time T to the "T time message" information in the waveform of Channel B in Figure 5 according to the rising edge of the signal received by Channel A in Figure 5 The time Δt128 at the beginning moment, and the time 29Δt required for the start and end of the "T time message" information in Figure 5 is measured, and (Δt1+Δt) is obtained; the pulse signal output terminal 4 of the controllable time scale signal source 1 is closed in Figure 4 The pulse output signal of the oscilloscope 2 is set to trigger the display mode of the rising edge of the pulse input signal on channel A;

图7的串行报文测试第四步46:设定图4可控时标信号源1的脉冲信号输出端4的脉冲输出开放时间T,并置为到时触发方式(指定T时刻27为图5所示通道A期望捕捉的指定P_1pps信号在指定时刻的卫星同步脉冲上升沿),设定图4可控时标信号源1可控开关S5断开时间0为(T+ΔT),其中ΔT与本检测步骤第三步得到的(Δt1+Δt)相关,(Δt1+Δt)<ΔT<1sec;The fourth step 46 of the serial message test of Fig. 7: set the pulse output opening time T of the pulse signal output terminal 4 of the controllable time scale signal source 1 in Fig. 4, and set it as the trigger mode when it arrives (designate T moment 27 as The specified P_1pps signal that channel A expects to capture as shown in Figure 5 is at the rising edge of the satellite synchronous pulse at the specified moment), and the controllable time scale signal source 1 controllable switch S5 disconnection time 0 in Figure 4 is set to be (T+ΔT), wherein ΔT is related to (Δt1+Δt) obtained in the third step of this detection step, (Δt1+Δt)<ΔT<1sec;

图7的串行报文测试第五步47:图4中可控时标信号源1的脉冲信号输出端4,输出T时刻卫星同步脉冲起始的1pps,通过图4示波器2的通道A、B可捕获到图5“T时间报文”信息波形32;The fifth step 47 of the serial message test in Fig. 7: the pulse signal output terminal 4 of the controllable time scale signal source 1 in Fig. 4, output 1pps of the satellite synchronous pulse start at T moment, pass through the channel A of Fig. 4 oscilloscope 2, B can capture the information waveform 32 of the "T time message" in Figure 5;

图7的串行报文测试第六步48:图4可控时标信号源1的可控开关S5在(T+ΔT)时刻断开、卫星同步授时装置3的串行报文输出端X1端12至通信转换器输入端C1端16的连接被切断、计算机9的串行报文信息接收被停止;图4中计算机9最后接收的串行报文信息,即为本串行报文测试第五步47中“T时间报文”信息波形32的信息帧内容,也即为T时刻后的第一个串行报文数据帧;图4中计算机9接收的倒数第二个串行报文信息,即为T时刻前的最后一个串行报文数据帧“T-1sec时间报文”信息。The sixth step 48 of the serial message test in Fig. 7: the controllable switch S5 of the controllable time scale signal source 1 in Fig. 4 is disconnected at (T+ΔT) moment, the serial message output terminal X1 of the satellite synchronous timing device 3 The connection between terminal 12 and terminal 16 of communication converter input terminal C1 is cut off, and the serial message information reception of computer 9 is stopped; the serial message information received by computer 9 in Fig. 4 is the serial message test The information frame content of " T time message " information waveform 32 in the 5th step 47, also is the first serial message data frame after T moment; The penultimate serial message that computer 9 receives among Fig. 4 The message information is the information of the last serial message data frame "T-1sec time message" before the time T.

测试结束。The test is over.

Claims (7)

1. the temporal information detection method of the synchronous time service device output signal of satellite is characterized in that: " T time message " information of being tested collects from computing machine (9) through following steps:
1., gauge tap S (5) closure in controlled timing signal source, computing machine (9) is in the message information state that the serial message output terminal X (12,13) of the synchronous time service device of normal reception satellite is exported;
2., set the output open hour T of the pulse signal output end (4) in controlled timing signal source (1), and being changed to triggering mode then, gauge tap S (5) disconnection of setting controlled timing signal source is to specify the action initial delay time Δ T (25) of the T moment (27)+gauge tap S constantly constantly;
3., the T initial 1pps of (27) output T moment satellite synchronizing pulse is constantly being specified in controlled timing signal source (1);
4., at the action initial delay time Δ T (25) that specifies the T moment (27)+gauge tap S constantly, disconnect the gauge tap S (5) in controlled timing signal source, first serial message data frame that computing machine (9) finally received after the appointment T moment (27) is " T time message " information, and preceding final data frame of the appointment T moment (27) is " T-1sec time message " information.
2. the temporal information detection method of the synchronous time service device output signal of satellite according to claim 1, it is characterized in that: the T initial 1pps of (27) output T moment satellite synchronizing pulse is constantly being specified in described controlled timing signal source (1), passage A, the B of oscillograph (2) captures " T time message " information waveform (32), and be carved into the time Δ t1 (28) in " T time message " the initial moment of information when recording T thus, and T time message information rises, end required time Δ t (29).
3. the temporal information detection method of the synchronous time service device output signal of satellite according to claim 1, it is characterized in that: the action initial delay time Δ T (25) of described gauge tap S is (time Δ t1 (the 28)+T time message information that is carved into " T time message " the initial moment of information during T plays, ends required time Δ t (29)), measure at random according to the rising edge of the appointment T moment (27) signal of passage A reception by oscillograph (2), before " T time message " information of collection, obtain in advance.
4. the temporal information detection method of the synchronous time service device output signal of satellite according to claim 1, it is characterized in that: the action initial delay time Δ T (25) of described gauge tap S in following time range, (time Δ t1 (28)+" T time message " information that is carved into " T time message " the initial moment of information during T rise, end required time Δ t (29))<Δ T<1 second.
5. the temporal information detection method of the synchronous time service device output signal of satellite according to claim 1, it is characterized in that: described controlled timing signal source (1) can be a monopulse at the pulse signal of specifying the T moment (27) to send, and also can be the frequency pulse signal.
6. the temporal information detection method of the synchronous time service device output signal of satellite, it is characterized in that: described T time IRIG-B coding waveforms (33) temporal information is checked by following steps:
1., close the output of the pulse signal output end (4) in controlled timing signal source (1), it is that the pulse input signal rising edge triggers display mode that oscillograph (2) is provided with passage A;
2., the pulse signal output end (4) of setting controlled timing signal source (1) is exported open hour T and is changed to triggering mode then;
3., the output of the pulse signal output end (4) in controlled timing signal source (1) specifies the T initial 1pps of satellite synchronizing pulse of (27) constantly, captures the IRIG-B coding waveforms (33) of T time by passage A, the C of oscillograph (2);
4., according to T time IRIG-B coding waveforms (33) information readout time, relatively itself and controlled timing signal source (1) set the consistance of time T.
7. the temporal information detection method of the synchronous time service device output signal of satellite according to claim 6, it is characterized in that: described controlled timing signal source (1) can be a single pulse signal at the pulse signal of specifying the T moment (27) to send, and also can be the frequency pulse signal.
CN 200810047989 2008-06-12 2008-06-12 Time information detection method of output signal of satellite synchronous timing device Active CN101604142B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200810047989 CN101604142B (en) 2008-06-12 2008-06-12 Time information detection method of output signal of satellite synchronous timing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200810047989 CN101604142B (en) 2008-06-12 2008-06-12 Time information detection method of output signal of satellite synchronous timing device

Related Child Applications (1)

Application Number Title Priority Date Filing Date
CN 201010293771 Division CN101957593B (en) 2008-06-12 2008-06-12 Time information detection method of output signal of satellite synchronization time service device

Publications (2)

Publication Number Publication Date
CN101604142A true CN101604142A (en) 2009-12-16
CN101604142B CN101604142B (en) 2011-02-09

Family

ID=41469906

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200810047989 Active CN101604142B (en) 2008-06-12 2008-06-12 Time information detection method of output signal of satellite synchronous timing device

Country Status (1)

Country Link
CN (1) CN101604142B (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101738931B (en) * 2009-12-24 2012-03-21 华北电力大学 IRIG-B (Inter-Range Instrumentation Group-B) code time hack device and time hack method thereof
CN102590619A (en) * 2012-03-14 2012-07-18 湖北省电力公司电力试验研究院 Method for detecting time synchronization capacity of real-time measurement equipment based on timing variable
CN102593955A (en) * 2012-03-05 2012-07-18 广西电网公司电力科学研究院 Comprehensive intelligent time frequency testing system and testing method
CN102591194A (en) * 2012-03-06 2012-07-18 广西电网公司电力科学研究院 Intelligent test system and method used for IRIG (Inter-range Instrumentation Group)-B code fault-tolerant function of time synchronizer
CN102638102A (en) * 2012-04-02 2012-08-15 安徽立卓智能电网科技有限公司 Power supply system key information acquisition system and communication method based on Beidou satellite transmission and communication method thereof
CN103529690A (en) * 2013-11-01 2014-01-22 西安邮电大学 Wall clock for receiving Beidou satellite time and wall clock time calibrating method
CN104683090A (en) * 2015-03-19 2015-06-03 浙江赛思电子科技有限公司 Expandable clock monitoring device and method
CN104882962A (en) * 2015-04-21 2015-09-02 国家电网公司 Information acquisition monitoring system based on BeiDou satellite and information acquisition method based on BeiDou satellite
CN105376044A (en) * 2015-12-08 2016-03-02 南京讯汇科技发展有限公司 Secondary equipment time monitoring system and method for power system
CN103957069B (en) * 2014-05-14 2016-08-24 国家电网公司 Time calibration in network IED time synchronized detection method based on physical layer time information
CN106502233A (en) * 2016-09-29 2017-03-15 北京广利核系统工程有限公司 A kind of nuclear plant digital I&C system calibration method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1455489A (en) * 2003-06-03 2003-11-12 东南大学 Satellite synchronous time apparatus for power system
FR2863814B1 (en) * 2003-12-16 2006-04-28 Cit Alcatel METHOD OF UPDATING THE BIT OF CLOCK EXISTING BETWEEN A BTS STATION OF A GSM NETWORK AND THE SATELLITES OF A GPS SYSTEM
CN100395682C (en) * 2004-10-20 2008-06-18 清华大学 Method and device for mutual standby time service using Beidou satellite navigation system and global positioning system
US7616153B2 (en) * 2006-08-04 2009-11-10 Seiko Epson Corporation Electronic device and time adjustment method

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101738931B (en) * 2009-12-24 2012-03-21 华北电力大学 IRIG-B (Inter-Range Instrumentation Group-B) code time hack device and time hack method thereof
CN102593955A (en) * 2012-03-05 2012-07-18 广西电网公司电力科学研究院 Comprehensive intelligent time frequency testing system and testing method
CN102593955B (en) * 2012-03-05 2014-01-01 广西电网公司电力科学研究院 Comprehensive intelligent time frequency testing system and testing method
CN102591194A (en) * 2012-03-06 2012-07-18 广西电网公司电力科学研究院 Intelligent test system and method used for IRIG (Inter-range Instrumentation Group)-B code fault-tolerant function of time synchronizer
CN102591194B (en) * 2012-03-06 2013-06-19 广西电网公司电力科学研究院 Intelligent test system and method used for IRIG (Inter-range Instrumentation Group)-B code fault-tolerant function of time synchronizer
US9257039B2 (en) 2012-03-14 2016-02-09 State Grid Corporation Of China Method for detecting time synchronization ability of real-time measuring device based on time variable
CN102590619A (en) * 2012-03-14 2012-07-18 湖北省电力公司电力试验研究院 Method for detecting time synchronization capacity of real-time measurement equipment based on timing variable
WO2013135069A1 (en) * 2012-03-14 2013-09-19 湖北省电力公司电力科学研究院 Timing variable based method for detecting time synchronization capability of real-time measurement device
CN102638102A (en) * 2012-04-02 2012-08-15 安徽立卓智能电网科技有限公司 Power supply system key information acquisition system and communication method based on Beidou satellite transmission and communication method thereof
CN103529690A (en) * 2013-11-01 2014-01-22 西安邮电大学 Wall clock for receiving Beidou satellite time and wall clock time calibrating method
CN103957069B (en) * 2014-05-14 2016-08-24 国家电网公司 Time calibration in network IED time synchronized detection method based on physical layer time information
CN104683090A (en) * 2015-03-19 2015-06-03 浙江赛思电子科技有限公司 Expandable clock monitoring device and method
CN104882962A (en) * 2015-04-21 2015-09-02 国家电网公司 Information acquisition monitoring system based on BeiDou satellite and information acquisition method based on BeiDou satellite
CN105376044A (en) * 2015-12-08 2016-03-02 南京讯汇科技发展有限公司 Secondary equipment time monitoring system and method for power system
CN106502233A (en) * 2016-09-29 2017-03-15 北京广利核系统工程有限公司 A kind of nuclear plant digital I&C system calibration method
CN106502233B (en) * 2016-09-29 2019-06-07 北京广利核系统工程有限公司 A kind of nuclear plant digital I&C system calibration method

Also Published As

Publication number Publication date
CN101604142B (en) 2011-02-09

Similar Documents

Publication Publication Date Title
CN101604142B (en) Time information detection method of output signal of satellite synchronous timing device
CN102590619B (en) Time synchronization ability detection method of real-time measurement equipment based on timing variables
CN104102122B (en) A kind of hand-held time synchronization tester
CN104076321B (en) On-line monitoring and evaluating system and method for digital electric energy meter
CN104215838B (en) Remote nuclear phase method for intelligent substation
CN203259610U (en) Merging unit accurate time testing instrument based on analog signal digital transmission
CN109683117A (en) Flexible direct current electronic type voltage transformer transient state step response test macro
CN204065388U (en) A wireless detection device for secondary circuit voltage drop of voltage transformer
CN202383278U (en) Merging unit sampling value time delay measuring system
CN101957593B (en) Time information detection method of output signal of satellite synchronization time service device
CN105548769A (en) Relay protection action delay time grading test system and method
CN103293414A (en) Intelligent substation protection device synchronization performance test system and method based on GPS (globe positioning system) accurate time synchronization technology
CN201740842U (en) Digital fault oscilloscope
CN104297593B (en) Punctuality error detection method for intelligent substation merging unit
CN106054000B (en) It is spaced combining unit power-factor angle consistency on-site test system and test method
CN103905045B (en) Alternating-current analog-digital conversion device real-time response detection method based on physical layer sampled value
CN107819466A (en) Sampled value signal time synchronization detecting method based on exchange analog-to-digital conversion real-time response
CN204256149U (en) A kind of Performance Test System of merge cells tester
CN206411250U (en) A kind of DC electronic current transformer digitizes real-time calibration equipment
CN103595582B (en) High-accuracy synchronous system detection device applied to intelligent transformer substation
CN201740861U (en) Current transformer calibrator based on IEC 61850 standard
CN204925260U (en) Intelligent substation small -signal communication test equipment
CN201887543U (en) Sampling value time calibration device
CN205103330U (en) Portable fault oscillograph of electrified installation
CN106371046A (en) Device for detecting angle difference resolution of merging unit tester

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: STATE ELECTRIC NET CROP.

Effective date: 20121018

Owner name: THE ELECTRIC POWER SCIENCE RESEARCH INSTITUTE OF H

Free format text: FORMER OWNER: HUBEI PROV. POWER TEST INST.

Effective date: 20121018

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20121018

Address after: 430077, 361 East Main Street, Wuchang District, Hubei, Wuhan

Patentee after: Hubei Electric Power Research Institute of Power Company

Patentee after: State Grid Corporation of China

Address before: 430077, 361 East Main Street, Wuchang District, Hubei, Wuhan

Patentee before: Hubei Prov. Power Test Inst.