CN201654495U - Satellite timing machine - Google Patents
Satellite timing machine Download PDFInfo
- Publication number
- CN201654495U CN201654495U CN 201020167086 CN201020167086U CN201654495U CN 201654495 U CN201654495 U CN 201654495U CN 201020167086 CN201020167086 CN 201020167086 CN 201020167086 U CN201020167086 U CN 201020167086U CN 201654495 U CN201654495 U CN 201654495U
- Authority
- CN
- China
- Prior art keywords
- time
- circuit
- time service
- satellite
- microcontroller
- 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.)
- Expired - Lifetime
Links
- 230000005540 biological transmission Effects 0.000 claims abstract description 33
- 238000004891 communication Methods 0.000 claims description 42
- 238000001914 filtration Methods 0.000 claims description 6
- 230000001360 synchronised effect Effects 0.000 claims description 3
- 230000002123 temporal effect Effects 0.000 claims 5
- 238000005259 measurement Methods 0.000 abstract description 23
- 238000009434 installation Methods 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 16
- 230000008569 process Effects 0.000 description 15
- 238000010586 diagram Methods 0.000 description 8
- 101000822028 Homo sapiens Solute carrier family 28 member 3 Proteins 0.000 description 5
- 102100021470 Solute carrier family 28 member 3 Human genes 0.000 description 5
- 230000006872 improvement Effects 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 101000685663 Homo sapiens Sodium/nucleoside cotransporter 1 Proteins 0.000 description 1
- 101000821827 Homo sapiens Sodium/nucleoside cotransporter 2 Proteins 0.000 description 1
- 102100023116 Sodium/nucleoside cotransporter 1 Human genes 0.000 description 1
- 102100021541 Sodium/nucleoside cotransporter 2 Human genes 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Images
Landscapes
- Electric Clocks (AREA)
Abstract
本实用新型公开了一种卫星授时一体机。本实用新型将用于卫星授时的远端与近端集成为一体、并利用线缆与被授时设备交互差分信号,由于差分信号的可靠传送距离大于单端电气特性信号,因而即便与被授时设备之间的线缆传送距离大于10米,也能够保证时标信号和时间信息的有效传送,同时,本实用新型还通过对线缆时延的测量、以及依据测量结果对时标信号的时延校准,减少由传送距离的扩展而导致的时标信号误差,因而还能够确保时标信号的准确传送;而且,由于远端与近端集成为一体,因而也不存在远端与近端之间的射频电缆长度超过100米所导致的各类问题。从而,本实用新型能够同时确保工程安装的便利、以及授时的可靠性。
The utility model discloses a satellite time service integrated machine. The utility model integrates the remote end and the near end used for satellite timing, and uses cables to exchange differential signals with the timed equipment. Since the reliable transmission distance of the differential signal is greater than that of the single-ended electrical characteristic signal, even with the timed equipment The cable transmission distance between them is greater than 10 meters, which can also ensure the effective transmission of time scale signals and time information. At the same time, the utility model also measures the time delay of the cables and the time delay of the time scale signals according to the measurement results. Calibration can reduce the time scale signal error caused by the extension of the transmission distance, so it can also ensure the accurate transmission of the time scale signal; moreover, because the far end and the near end are integrated, there is no gap between the far end and the near end. Various problems caused by the RF cable length exceeding 100 meters. Therefore, the utility model can simultaneously ensure the convenience of engineering installation and the reliability of timing.
Description
技术领域technical field
本实用新型涉及卫星授时技术,特别涉及一种卫星授时一体机。The utility model relates to satellite time service technology, in particular to a satellite time service integrated machine.
背景技术Background technique
在现代通信、测控系统中需要多个设备之间时间系统之间长期保持相互同步,且同步精度需要达到亚微秒(us)级甚至纳秒(ns)级。目前能够达到亚us级或ns级同步精度的授时方案包括地面有线授时系统和卫星授时两种方式。其中,地面有线授时网络一般为局域授时专网,但受到网络部署区域和网络私有两方面限制无法得到广泛应用;而卫星授时则具有开放性、覆盖广、精度高、成本低等特点因而得到广泛的应用。In modern communication and measurement and control systems, it is necessary for multiple devices to maintain mutual synchronization between the time systems for a long time, and the synchronization accuracy needs to reach the sub-microsecond (us) level or even nanosecond (ns) level. At present, the timing schemes that can achieve sub-us level or ns level synchronization accuracy include ground wired timing system and satellite timing. Among them, the ground wired time service network is generally a local time service private network, but it cannot be widely used due to the limitations of the network deployment area and network privateness; while the satellite time service has the characteristics of openness, wide coverage, high precision, and low cost. Wide range of applications.
图1简易示出了现有的一种分体式卫星授时设备,其至少包括远端的外置GPS天线110、以及近端的GPS星卡120,远端与近端之间通过射频电缆130实现GPS天线110到GPS星卡120的射频信号传送、以及GPS星卡120对天线110的电源馈电。其中,远端的外置GPS天线110至少包括单模的天线馈源111、滤波电路112等,而近端的GPS星卡120则具有单模的定位解算功能,用以从来自GPS天线110的卫星信号中定位解算出时标信号(1PPS)和时间信息(TOD),并将时标信号和时间信息通过单端电气特性信号140发送至被授时设备,实现对被授时设备的授时。Figure 1 simply shows an existing split-type satellite timing device, which at least includes a remote
然而,由于近端的GPS星卡120与被授时设备之间采用单端电气特性信号140、即仅以地为参考的信号,因而为了避免传递的信号受干扰,只能将近端的GPS星卡120与被授时设备之间传送距离限制在10米以内。However, since the near-end
此外,由于射频线缆会导致损耗,因而远端与近端之间的射频电缆长度也不能超过100米。从而,在需要同时确保近端的星卡与被授时设备之间传送距离不超过10米、以及远端与近端之间的射频线缆长度不超过100米的情况下,会使得远端和近端的工程安装较为困难;反之,如果在工程安装时不能确保上述的距离限制,则会由于不满足理想工作条件,而使导致分体式卫星授时设备对被授时设备的授时可靠性大大降低。In addition, the length of the RF cable between the far end and the near end cannot exceed 100 meters because of the loss caused by the RF cable. Therefore, when it is necessary to ensure that the transmission distance between the near-end star card and the timed device does not exceed 10 meters, and the length of the radio frequency cable between the far-end and the near-end does not exceed 100 meters, it will make the far-end and the near-end The near-end engineering installation is more difficult; on the contrary, if the above-mentioned distance limit cannot be ensured during engineering installation, the timing reliability of the split satellite timing equipment to the timing equipment will be greatly reduced due to the unsatisfied ideal working conditions.
实用新型内容Utility model content
有鉴于此,本实用新型提供了一种卫星授时一体机,能够扩展卫星授时一体机与被授时设备之间的物理距离。In view of this, the utility model provides a satellite time service integrated machine, which can extend the physical distance between the satellite time service integrated machine and the timed equipment.
本实用新型提供的一种卫星授时一体机,包括:The utility model provides a satellite time service integrated machine, comprising:
天线,其接收卫星信号;an antenna, which receives satellite signals;
滤波电路,其对天线接收到的卫星信号进行滤波的滤波电路;A filter circuit, which filters satellite signals received by the antenna;
定位解算电路,其对滤波后的卫星信号进行定位解算、并得到时标信号和时间信息,将得到的时标信号发送至时延补偿电路和微控制器;A positioning calculation circuit, which performs positioning calculation on the filtered satellite signal, obtains a time scale signal and time information, and sends the obtained time scale signal to the time delay compensation circuit and the microcontroller;
还包括:微控制器、测量电路、时延补偿电路、差分通信电路,其中:Also includes: a microcontroller, a measurement circuit, a delay compensation circuit, a differential communication circuit, wherein:
测量电路,其通过差分通信电路与被授时设备交互校准序列,并观测发送校准序列的本端时间、以及被授时设备反馈的校准序列的本端接收时间;A measurement circuit, which interacts with the timing device through the differential communication circuit for the calibration sequence, and observes the local time of sending the calibration sequence and the local receiving time of the calibration sequence fed back by the timing device;
时延补偿电路,其根据测量电路收发校准序列的时间、以及被授时设备收发校准序列的时间,对定位解算电路得到的时标信号进行校准,并将校准后的时标信号通过差分通信电路发送至被授时设备;Delay compensation circuit, which calibrates the time scale signal obtained by the positioning solution circuit according to the time when the measurement circuit sends and receives the calibration sequence and the time when the time service device receives and receives the calibration sequence, and passes the calibrated time scale signal through the differential communication circuit Send to the timed device;
微控制器,其依据定位解算电路得到的时标信号,将定位解算电路得到的对应时间信息通过差分通信电路发送至被授时设备、并使该时间信息与校准后的对应时标信号同步发送,还通过差分通信电路向被授时设备通告测量电路接收校准序列的时间、并接收被授时设备通告的对端收发校准序列的时间;Microcontroller, which sends the corresponding time information obtained by the positioning resolving circuit to the timing device through the differential communication circuit according to the time scale signal obtained by the positioning resolving circuit, and synchronizes the time information with the calibrated corresponding time scale signal Sending, and also notifying the timing device through the differential communication circuit of the time when the measurement circuit receives the calibration sequence, and receiving the time when the opposite end sends and receives the calibration sequence notified by the timing device;
差分通信电路,其通过线缆与被授时设备交互差分信号。The differential communication circuit exchanges differential signals with the timed equipment through cables.
微控制器进一步控制差分通信电路的收发状态,使差分通信电路以半双工方式通过线缆与被授时设备交互差分信号。The microcontroller further controls the sending and receiving state of the differential communication circuit, so that the differential communication circuit exchanges differential signals with the timed device through cables in a half-duplex manner.
定位解算电路、测量电路、时延补偿电路、差分通信电路挂接于微控制器总线,且,定位解算电路进一步通过直连信号线分别与微控制器和时延补偿电路相连、并通过直连信号线将时标信号发送至微控制器和时延补偿电路。The positioning calculation circuit, the measurement circuit, the delay compensation circuit, and the differential communication circuit are connected to the microcontroller bus, and the positioning calculation circuit is further connected to the microcontroller and the delay compensation circuit through a direct connection signal line, and through A direct signal line sends the timing signal to the microcontroller and the skew compensation circuit.
测量电路包括:The measurement circuit consists of:
校准序列产生器,其产生校准序列、并通过差分通信电路发送至被授时设备;A calibration sequence generator, which generates a calibration sequence and sends it to the timed device through a differential communication circuit;
发送时间观测器,其观测校准序列产生器所产生的校准序列的本端发送时间、并通过微控制器总线发送至时延补偿电路;A sending time observer, which observes the local sending time of the calibration sequence generated by the calibration sequence generator, and sends it to the delay compensation circuit through the microcontroller bus;
接收时间观测器,其通过差分通信电路接收被授时设备反馈的校准序列、并观测该校准序列的本端接收时间,然后通过微控制器总线发送至时延补偿电路。The receiving time observer receives the calibration sequence fed back by the timing device through the differential communication circuit, observes the local receiving time of the calibration sequence, and then sends it to the delay compensation circuit through the microcontroller bus.
校准序列产生器与发送时间观测器通过直连信号线相连、接收时间观测器与差分通信电路通过直连信号线相连。The calibration sequence generator is connected to the sending time observer through a direct connection signal line, and the receiving time observer is connected to the differential communication circuit through a direct connection signal line.
差分通信电路包括:Differential communication circuits include:
发送选择器,其选择校准序列产生器产生的校准序列、以及时延补偿电路校准后的时标信号中的一路发送至第一半双工差分收发器;A transmission selector, which selects one of the calibration sequence generated by the calibration sequence generator and the time scale signal calibrated by the delay compensation circuit to send to the first half-duplex differential transceiver;
第一半双工差分收发器,其通过线缆将发送选择器所选择的一路以差分信号的方式发送至被授时设备,还将通过线缆接收到的被授时设备反馈的校准序列发送至接收时间观测器;The first half-duplex differential transceiver sends the channel selected by the transmission selector to the timed device in the form of a differential signal through the cable, and sends the calibration sequence fed back by the timed device received through the cable to the receiver time observer;
第一收发控制器,其挂接于微控制器总线、以受控于微控制器,并在需要测量电缆时延时控制发送选择器选择校准序列产生器产生的校准序列、在需要校准时控制发送选择器选择时延补偿电路校准后的时标信号,以及,控制第一半双工差分收发器的收发状态;The first transceiver controller, which is connected to the microcontroller bus, is controlled by the microcontroller, and controls the transmission selector to select the calibration sequence generated by the calibration sequence generator when the cable needs to be measured, and controls when calibration is required. The transmit selector selects the time scale signal calibrated by the delay compensation circuit, and controls the transmitting and receiving state of the first half-duplex differential transceiver;
第二半双工差分收发器,其将通过线缆接收到的被授时设备的前述通告发送至微控制器,还将来自微控制器的前述通告以差分信号的方式发送至被授时设备;The second half-duplex differential transceiver, which sends the aforementioned notification of the timed device received through the cable to the microcontroller, and also sends the aforementioned notification from the microcontroller to the timed device in the form of a differential signal;
第二收发控制器,其挂接于微控制器总线、以受控于微控制器,并控制第二半双工差分收发器的收发状态。The second transceiver controller is connected to the microcontroller bus to be controlled by the microcontroller, and controls the transceiver state of the second half-duplex differential transceiver.
所述线缆包括:The cables include:
第一半双工差分收发器的1根电源线、1根接地线、以及2根差分信号线;1 power line, 1 ground line, and 2 differential signal lines of the first half-duplex differential transceiver;
第二半双工差分收发器的1根电源线、1根接地线、以及2根差分信号线。One power line, one ground line, and two differential signal lines of the second half-duplex differential transceiver.
第一收发控制器进一步在需要测量电缆时延时触发校准序列产生器、或触发发送时间观测器。The first transceiver controller further triggers the calibration sequence generator or triggers the transmission time observer when the cable time delay needs to be measured.
天线为多模天线、定位解算电路为多模定位解算电路。The antenna is a multi-mode antenna, and the positioning calculation circuit is a multi-mode positioning calculation circuit.
时间信息在校准后的对应时标信号发送之后的一秒内发送,以保证该时间信息与校准后的对应时标信号同步发送。。The time information is sent within one second after the calibrated corresponding time scale signal is sent, so as to ensure that the time information is sent synchronously with the calibrated corresponding time scale signal. .
由上述技术方案可见,本实用新型将用于卫星授时的远端与近端集成为一体、并利用线缆与被授时设备交互差分信号,由于差分信号的可靠传送距离大于单端电气特性信号,因而即便与被授时设备之间的线缆传送距离大于10米,也能够保证时标信号和时间信息的有效传送,同时,本实用新型还通过对线缆时延的测量、以及依据测量结果对时标信号的时延校准,减少由传送距离的扩展而导致的时标信号误差,因而还能够确保时标信号的准确传送;而且,由于远端与近端集成为一体,因而也不存在远端与近端之间的射频电缆长度超过100米所导致的各类问题。从而,本实用新型能够同时确保工程安装的便利、以及授时的可靠性。进一步地,本实用新型可以采用半双工方式复用线缆。It can be seen from the above technical solution that the utility model integrates the remote and near ends used for satellite timing, and uses cables to exchange differential signals with timed equipment. Since the reliable transmission distance of differential signals is greater than that of single-ended electrical characteristic signals, Therefore, even if the cable transmission distance between the time-serving equipment is greater than 10 meters, it can also ensure the effective transmission of time scale signals and time information. The time-delay calibration of the time-scale signal reduces the time-scale signal error caused by the extension of the transmission distance, thus ensuring the accurate transmission of the time-scale signal; moreover, since the far-end and the near-end are integrated, there is no remote Various problems caused by the length of the RF cable between the end and the near end exceeding 100 meters. Therefore, the utility model can simultaneously ensure the convenience of engineering installation and the reliability of timing. Further, the utility model can use a half-duplex mode to multiplex cables.
附图说明Description of drawings
图1为现有技术中的一种分体式卫星授时设备的简易结构示意图;Fig. 1 is a simple structure schematic diagram of a split type satellite timing device in the prior art;
图2为本实用新型实施例中卫星授时一体机的示例性结构示意图;Fig. 2 is the exemplary structure schematic diagram of satellite time service all-in-one machine in the utility model embodiment;
图3为本实用新型实施例中卫星授时一体机的一种具体结构示意图;Fig. 3 is a kind of specific structural representation of satellite time service integrated machine in the utility model embodiment;
图4为本实用新型实施例中卫星授时一体机的另一种具体结构示意图;Fig. 4 is another kind of concrete structure schematic diagram of satellite time service integrated machine in the utility model embodiment;
图5为本实用新型实施例中卫星授时一体机测量过程的示例性流程图;Fig. 5 is an exemplary flow chart of the measurement process of the satellite timing service integrated machine in the embodiment of the present invention;
图6为本实用新型实施例中卫星授时一体机与被授时设备在测量过程中的交互时序图;Fig. 6 is the interaction sequence diagram of the integrated satellite timing machine and the timed equipment in the measurement process in the embodiment of the present invention;
图7为本实用新型实施例中卫星授时一体机授时过程的示例性流程图。Fig. 7 is an exemplary flow chart of the timing process of the integrated satellite timing machine in the embodiment of the present invention.
具体实施方式Detailed ways
为使本实用新型的目的、技术方案及优点更加清楚明白,以下参照附图并举实施例,对本实用新型进一步详细说明。In order to make the purpose, technical solutions and advantages of the utility model clearer, the utility model will be further described in detail below with reference to the accompanying drawings and examples.
本实施例将用于卫星授时的远端与近端集成为一体,并利用线缆与被授时设备交互差分信号,由于差分信号的可靠传送距离大于单端电气特性信号,因而即便与被授时设备之间的线缆传送距离大于10米,也能够保证时标信号和时间信息(本文所述的时间信息中,除了时间信息本身之外,还可以进一步包含例如导航定位信息、控制信息等等其他为本领域技术人员所知晓的信息)的有效传送,同时,本实施例还通过对线缆时延的测量、以及依据测量结果对时标信号的时延校准,减少由传送距离的扩展而导致的时标信号误差,因而还能够确保时标信号的准确传送;而且,由于远端与近端集成为一体,因而也不存在远端与近端之间的射频电缆长度超过100米所导致的各类问题。从而,能够同时确保工程安装的便利、以及授时的可靠性。In this embodiment, the far-end and the near-end used for satellite timing are integrated, and the cable is used to exchange differential signals with the timed equipment. Since the reliable transmission distance of the differential signal is greater than that of the single-ended electrical characteristic signal, even with the timed equipment The cable transmission distance between them is greater than 10 meters, and it can also ensure the time scale signal and time information (the time information described in this paper, in addition to the time information itself, can further include other information such as navigation and positioning information, control information, etc. information known to those skilled in the art), and at the same time, this embodiment also reduces the transmission distance caused by the extension of the transmission distance by measuring the cable delay and calibrating the delay of the time scale signal according to the measurement results. The time scale signal error can ensure the accurate transmission of the time scale signal; moreover, since the far end and the near end are integrated, there is no problem caused by the length of the radio frequency cable between the far end and the near end exceeding 100 meters. Various problems. Therefore, the convenience of engineering installation and the reliability of timing can be ensured at the same time.
图2为本实用新型实施例中卫星授时一体机的示例性结构示意图。如图2所示,本实施例中的卫星授时一体机包括;天线202、滤波电路203、定位解算电路204、微控制器205、测量电路206、时延补偿电路207、差分通信电路208,其中,定位解算电路204、测量电路206、时延补偿电路207、差分通信电路208挂接在微控制器205总线上,并与微控制器205相耦合。Fig. 2 is a schematic structural diagram of an exemplary satellite timing service integrated machine in an embodiment of the present invention. As shown in Figure 2, the integrated satellite time service machine in this embodiment includes:
天线202,其可以是如现有分体式卫星授时设备所采用的单模天线馈源、也可以是任一种多模天线,用于接收卫星信号;
滤波电路203,其可以是现有任一种具有滤波功能的电路,用于对天线202接收到的卫星信号进行滤波的逻辑或物理电路;
定位解算电路204,其可以是任一种针对单模天线馈源的具有单模定位结算功能的逻辑或物理电路、也可以是任一种针对多模天线的具有多模定位结算功能的逻辑或物理电路,用于对滤波电路203滤波后的卫星信号进行定位解算、并得到时标信号和时间信息,将得到的时标信号发送至时延补偿电路207和微控制器205;
测量电路206,其可以是按照任一种方式校准序列、并具有时间记录功能的逻辑电路,用于通过差分通信电路208与被授时设备交互校准序列,并观测发送校准序列的本端时间、以及被授时设备反馈的校准序列的本端接收时间;Measuring
时延补偿电路207,其可以为可按照现有双向时延补偿原理实现延时补偿运算的逻辑电路,用于根据测量电路206收发校准序列的本端时间、以及被授时设备通告的对端收发校准序列的时间,对定位解算电路204得到的时标信号进行校准(具体的校准过程所依据的双向时延补偿原理属于现有技术、在此不再予以赘述),并将校准后的时标信号通过差分通信电路208发送至被授时设备;
微控制器205,其可以是任一种具有控制功能的逻辑电路,用于依据定位解算电路204得到的时标信号,将定位解算电路204得到的对应时间信息通过差分通信电路208发送至被授时设备、并使该时间信息与时延补偿电路207校准后的对应时标信号同步发送,还通过差分通信电路208向被授时设备通告测量电路206接收校准序列的时间、并接收被授时设备通告的对端收发校准序列的时间;其中,本文所述的时间信息与校准后的对应时标信号的同步发送,主要是指时间信息在校准后的对应时标信号发送之后的1秒内发送;
差分通信电路208,其通过线缆与被授时设备交互差分信号。A
此外,在如图1所示的卫星授时一体机中,为了避免时延补偿电路207和微控制器205从定位解算电路204得到的时标信号,由于通过微控制器205总线传输而产生的误差,定位解算电路204可以进一步通过直连信号线分别与微控制器205和时延补偿电路207相连、并通过直连信号线将时标信号发送至微控制器205和时延补偿电路207。In addition, in the integrated satellite time service machine shown in Figure 1, in order to avoid the time scale signal obtained by the time
较佳地,在如图1所示的卫星授时一体机中,微控制器205可以进一步控制差分通信电路208的收发状态,使差分通信电路208以半双工方式通过线缆与被授时设备交互差分信号,从而实现对线缆的复用。Preferably, in the satellite time service integrated machine as shown in Figure 1, the
实际应用中,如图1所示的卫星授时一体机中,除了天线202之外的其他部分均可以承载于同一个可编程逻辑芯片、或两个左右的可编程逻辑芯片中,当然,也可以每部分分别由一个可编程逻辑芯片、或相应的物理电路来实现。除了多种可选的物理实体实现方式,具体的逻辑电路结构或物理电路结构也是存在多种可选方式。In practical applications, in the integrated satellite time service machine shown in Figure 1, other parts except the
以下,就针对测量电路和差分通信电路具体的结构予以详细说明。Hereinafter, specific structures of the measuring circuit and the differential communication circuit will be described in detail.
图3为本实用新型实施例中卫星授时一体机的一种具体结构示意图。在图3中,测量电路306包括:校准序列产生器、发送时间观测器、接收时间观测器。Fig. 3 is a specific structural diagram of the satellite timing service integrated machine in the embodiment of the utility model. In FIG. 3 , the
校准序列产生器,其产生校准序列、并通过差分通信电路308发送至被授时设备;A calibration sequence generator, which generates a calibration sequence and sends it to the timed device through the
发送时间观测器,其与校准序列产生器通过直连信号线相连,用于观测校准序列产生器所产生的校准序列的本地发送时间、并将本地发送时间通过微控制器305总线发送至时延补偿电路307;Sending time observer, which is connected with the calibration sequence generator through a direct signal line, is used to observe the local sending time of the calibration sequence generated by the calibration sequence generator, and send the local sending time to the time delay through the
接收时间观测器,其与差分通信电路通过直连信号线相连,用于观测差分通信电路308接收被授时设备反馈的校准序列的本地接收时间、并将本地接收时间通过微控制器305总线发送至时延补偿电路307。The receiving time observer is connected with the differential communication circuit through a direct signal line, and is used to observe the local receiving time of the calibration sequence fed back by the timing device feedback by the
差分通信电路308包括:发送选择器、半双工差分收发器1、收发控制器1、半双工差分收发器2、收发控制器2。The
发送选择器,其选择校准序列产生器产生的校准序列、以及时延补偿电路307校准后的时标信号中的一路发送至半双工差分收发器1;A transmission selector, which selects one of the calibration sequence generated by the calibration sequence generator and the time scale signal calibrated by the
半双工差分收发器1,其与校准序列产生器、接收时间观测器、收发控制器1通过直连信号线相连,用于通过线缆将发送选择器所选择的一路以差分信号的方式发送至被授时设备,还将通过线缆接收到的被授时设备反馈的校准序列发送至接收时间观测器;Half-duplex differential transceiver 1, which is connected to the calibration sequence generator, receiving time observer, and transceiver controller 1 through a direct connection signal line, and is used to transmit the channel selected by the transmission selector as a differential signal through a cable To the timed device, the calibration sequence received by the timed device fed back through the cable is also sent to the receiving time observer;
收发控制器1,其挂接于微控制器305总线、以受控于微控制器305,并依据微控制器305的指令,在需要测量电缆时延时通过CNT3控制发送选择器选择校准序列产生器产生的校准序列、并通过CNT3触发发送时间观测器,在需要校准时通过CNT3控制发送选择器选择时延补偿电路校准后的时标信号;以及,依据微控制器305的指令,通过CNT1控制半双工差分收发器1的收发状态;The transceiver controller 1 is connected to the
半双工差分收发器2,其与微控制器305、收发控制器1通过直连信号线相连,用于将通过线缆接收到的被授时设备的通告(即被授时设备通告的对端收发校准序列的时间)发送至微控制器305,还将来自微控制器305的通告(即向被授时设备通告的本端接收校准序列的时间)以差分信号的方式发送至被授时设备;Half-
收发控制器2,其挂接于微控制器305总线、以受控于微控制器305,并依据微控制器305的指令,通过CNT2控制半双工差分收发器2的收发状态。The
此外,对于采用8芯线缆的情况下,半双工差分收发器1的1根电源线、1根接地线、以及2根差分信号线;半双工差分收发器2的1根电源线、1根接地线、以及2根差分信号线。In addition, in the case of using an 8-core cable, one power line, one ground line, and two differential signal lines of the half-duplex differential transceiver 1; one power line, one ground line, and two differential signal lines of the half-
图4为本实用新型实施例中卫星授时一体机的另一种具体结构示意图。图4中所示的具体结构相比于图3,仅仅在于半双工差分收发器1的控制方式,即在图4中,收发控制器1,依据微控制器305的指令,在需要测量电缆时延时通过CNT3控制发送选择器选择校准序列产生器产生的校准序列、并通过CNT3触发校准序列产生器。Fig. 4 is another specific structural diagram of the integrated satellite time service machine in the embodiment of the present invention. Compared with Fig. 3, the specific structure shown in Fig. 4 lies only in the control mode of the half-duplex differential transceiver 1, that is, in Fig. 4, the transceiver controller 1, according to the instructions of the
基于上述如图1所示结构的原理性描述,以及上述如图3和图4所示的具体结构,本领域技术人员能够推导出卫星授时一体机的其他结构、以及被授时设备所需的改进,本文就不再一一予以赘述。Based on the above-mentioned principle description of the structure shown in Figure 1, and the above-mentioned specific structure shown in Figure 3 and Figure 4, those skilled in the art can deduce other structures of the satellite time service integrated machine and the improvement required by the time service equipment , this article will not repeat them one by one.
而且,对于任何的具体电路结构,本实施例中的卫星授时一体机的工作原理均相同。下面,对卫星授时一体机的基本工作原理进行详细说明。Moreover, for any specific circuit structure, the working principle of the satellite timing service integrated machine in this embodiment is the same. Next, the basic working principle of the satellite timing service integrated machine will be described in detail.
卫星授时一体机在整机上电启动后,首先需要进行整机初始化。具体的初始化过程包括:After the satellite timing service integrated machine is powered on and started, the whole machine needs to be initialized first. The specific initialization process includes:
设置定位解算电路的工作模式,例如,设置为多模的联合导航模式、或单模的GPS单北斗工作模式;Set the working mode of the positioning calculation circuit, for example, set to multi-mode joint navigation mode, or single-mode GPS single Beidou working mode;
设置差分通信电路的工作模式,例如,针对如图3和如图4所示的具体电路结构,可设置半双工差分收发器1所对应的线路1、以及半双工差分收发器2所对应的线路2均为“半双工”工作模式,或者将二者之一设置为“半双工”工作模式、另一个设置为“仅发送”模式。Set the working mode of the differential communication circuit. For example, for the specific circuit structure shown in Figure 3 and Figure 4, the line 1 corresponding to the half-duplex differential transceiver 1 and the line 1 corresponding to the half-
在初始化结束后,卫星授时一体机即可开始正常工作,具体包括用于时延校准的测量、以及基于时延校准的正常授时操作。After the initialization, the integrated satellite timing machine can start to work normally, specifically including the measurement for delay calibration and the normal timing operation based on delay calibration.
图5为本实用新型实施例中卫星授时一体机测量过程的示例性流程图。如图5所示,用于时延校准的测量包括如下步骤:Fig. 5 is an exemplary flow chart of the measurement process of the satellite timing service integrated machine in the embodiment of the present invention. As shown in Figure 5, the measurement for delay calibration includes the following steps:
步骤501,卫星授时一体机通过线缆以差分信号的方式与被授时设备交互校准序列,并观测发送校准序列的本端时间、以及被授时设备反馈的校准序列的本端接收时间。Step 501, the satellite timing service integrated machine communicates the calibration sequence with the time-service device in the form of a differential signal through a cable, and observes the local time of sending the calibration sequence and the local reception time of the calibration sequence fed back by the time-service device.
步骤502,卫星授时一体机通过线缆以差分信号的方式向被授时设备通告本端接收校准序列的时间、并接收被授时设备通告的对端收发校准序列的时间。In
至此,用于时延校准的测量的过程结束。So far, the measurement process for delay calibration ends.
上述用于时延校准的测量过程还可以看作是卫星授时一体机与被授时设备之间时延校准的协商过程。The above measurement process for delay calibration can also be regarded as a negotiation process of delay calibration between the satellite time service integrated machine and the time service equipment.
图6为本实用新型实施例中卫星授时一体机与被授时设备在测量过程中的交互时序图。如图6所示,以如图3和图4所示的具体电路结构为例,假设半双工差分收发器1、以及半双工差分收发器2的工作模式均为“半双工”,用于时延校准的测量包括如下交互过程:Fig. 6 is a sequence diagram of the interaction between the integrated satellite timing machine and the timed equipment in the measurement process in the embodiment of the present invention. As shown in Figure 6, taking the specific circuit structure shown in Figure 3 and Figure 4 as an example, assuming that the working modes of half-duplex differential transceiver 1 and half-
步骤601,卫星授时一体机设置半双工差分收发器1所对应的线路1、以及半双工差分收发器2所对应的线路2的收发状态均为发送状态。Step 601 , the satellite time service integrated machine sets the transmitting and receiving states of the line 1 corresponding to the half-duplex differential transceiver 1 and the
步骤602,被授时设备设置线路1、线路2的收发状态均为接收状态。In step 602, the timed device sets the sending and receiving states of line 1 and
步骤603,卫星授时一体机从线路1发送校准序列到被授时设备,并观测本端发送校准序列的时间。Step 603 , the satellite timing service integrated machine sends the calibration sequence to the timed device from line 1, and observes the time when the local terminal sends the calibration sequence.
步骤604,卫星授时一体机发送校准序列完成后,设置线路1和线路2的收发状态为接收状态。Step 604, after the satellite time service integrated machine completes the transmission and calibration sequence, set the transmitting and receiving state of line 1 and
步骤605,被授时设备检测来自对端的校准序列,并观测被授时设备接收校准序列的本端时间。Step 605, the timed device detects the calibration sequence from the opposite end, and observes the local time when the timed device receives the calibration sequence.
步骤606,被授时设备检测到校准序列后,将线路1和线路2的收发状态设置为发送状态。Step 606, after the time service device detects the calibration sequence, set the sending and receiving state of line 1 and
步骤607,被授时设备从线路1发送校准序列到卫星授时一体机。Step 607, the time service equipment sends the calibration sequence to the satellite time service integrated machine from the line 1.
步骤608,被授时设备发送完成后设置线路1的收发状态为接收状态。Step 608, after the timed device completes sending, set the sending and receiving state of line 1 to the receiving state.
步骤609,卫星授时一体机检测来自对端的校准序列。Step 609, the satellite timing service integrated machine detects the calibration sequence from the opposite end.
步骤610,卫星授时一体机检测到来自对端的校准序列后,将线路1的收发状态设置为发送状态。Step 610, after the satellite timing service integrated machine detects the calibration sequence from the opposite end, it sets the transmitting and receiving state of line 1 to the sending state.
步骤611,被授时设备从线路2向卫星授时一体机通告自身观测到的校准序列的本地接收时间。In step 611, the timed device notifies the local receiving time of the calibration sequence observed by itself to the satellite time service integrated machine from
步骤612,被授时设备从线路2通告本端向卫星授时一体机发送校准序列的本端发送时间。Step 612 , the time-serviced device notifies the local sending time of the calibration sequence sent by the local end to the satellite time service integrated machine through the
步骤613,被授时设备发送完成后设置线路2的收发状态为接收状态。Step 613, after the timed device completes sending, set the sending and receiving status of
步骤614,卫星授时一体机将线路2的收发状态设置为发送状态。In step 614, the integrated satellite time service unit sets the transmitting and receiving state of
步骤615,卫星授时一体机将本端接收被授时设备反馈的校准序列的本端收时间,通过线路2通告给被授时设备。Step 615 , the satellite time service integrated machine notifies the local receiving time of the calibration sequence fed back by the time service equipment at the local terminal to the time service equipment through
步骤616,卫星授时一体机根据本端收发校准序列的时间、以及被授时设备通告的对端收发校准序列的时间进行校准补偿,被授时设备根据本端收发校准序列的时间进行校准补偿。Step 616, the satellite time service integrated machine performs calibration compensation according to the time when the local end transmits and receives the calibration sequence and the time when the peer end transmits and receives the calibration sequence notified by the time service device, and the time service device performs calibration compensation according to the time when the local end transmits and receives the calibration sequence.
此后可选地,卫星授时一体机还可向被授时设备发送测试结束消息。Optionally thereafter, the integrated satellite time service unit can also send a test end message to the timed device.
至此,本流程结束。So far, this process ends.
在上述流程之后,卫星授时一体机即可正常授时模式,并以补偿后的时标信号对被授时设备进行授时,使输出的时标信号到达被授时设备输入口的时标与卫星时间源对齐,实现高精度授时。After the above process, the satellite time service integrated machine can be in the normal time service mode, and use the compensated time scale signal to perform time service to the time service equipment, so that the output time scale signal reaches the time scale of the input port of the time service equipment and aligns with the satellite time source , to achieve high-precision timing.
图7为本实用新型实施例中卫星授时一体机授时过程的示例性流程图。如图5所示,基于时延校准的正常授时操作包括循环执行的如下步骤:Fig. 7 is an exemplary flow chart of the timing process of the integrated satellite timing machine in the embodiment of the present invention. As shown in Figure 5, the normal timing operation based on delay calibration includes the following steps of cyclic execution:
步骤701,接收卫星信号;
步骤702,对接收到的卫星信号进行滤波;
步骤703,对滤波后的卫星信号进行定位解算、并得到时标信号和时间信息;
步骤704,根据本端收发校准序列的时间、以及被授时设备通告的对端收发校准序列的时间,对定位解算得到的时标信号进行校准,并通过线缆将校准后的时标信号以差分信号的方式发送至被授时设备;Step 704: Calibrate the time scale signal obtained from the positioning solution according to the time when the local end transmits and receives the calibration sequence and the time when the peer end transmits and receives the calibration sequence notified by the timing device, and transmits the calibrated time scale signal as The differential signal is sent to the timed device;
步骤705,还通过线缆将校准后的该时标信号所对应的时间信息,以差分信号的方式同步发送至被授时设备。In
本步骤中的同步,即是指时间信息在校准后的对应时标信号发送之后的一秒内发送。The synchronization in this step means that the time information is sent within one second after the calibrated corresponding time scale signal is sent.
至此,本流程结束。So far, this process ends.
以上所述仅为本实用新型的较佳实施例而已,并非用于限定本实用新型的保护范围。凡在本实用新型的精神和原则之内,所作的任何修改、等同替换以及改进等,均应包含在本实用新型的保护范围之内。The above descriptions are only preferred embodiments of the present utility model, and are not intended to limit the protection scope of the present utility model. Any modifications, equivalent replacements and improvements made within the spirit and principles of the present utility model shall be included in the protection scope of the present utility model.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201020167086 CN201654495U (en) | 2010-04-19 | 2010-04-19 | Satellite timing machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201020167086 CN201654495U (en) | 2010-04-19 | 2010-04-19 | Satellite timing machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201654495U true CN201654495U (en) | 2010-11-24 |
Family
ID=43119738
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201020167086 Expired - Lifetime CN201654495U (en) | 2010-04-19 | 2010-04-19 | Satellite timing machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201654495U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102035607A (en) * | 2010-12-08 | 2011-04-27 | 大唐移动通信设备有限公司 | Method and device for sending calibration data |
| CN102221818A (en) * | 2011-05-24 | 2011-10-19 | 国网电力科学研究院 | Transmission method for converting pulse time signals into differential bus signals by GPS (global positioning system) |
| CN102221816A (en) * | 2010-04-19 | 2011-10-19 | 普天信息技术研究院有限公司 | Satellite time serving all-in-one machine and time serving method thereof |
| CN105589328A (en) * | 2014-10-22 | 2016-05-18 | 中国移动通信集团公司 | Time synchronization test method and apparatus, and time synchronization testing precision determination method and apparatus |
| CN107070567A (en) * | 2017-04-06 | 2017-08-18 | 中国科学院国家授时中心 | Time delay calibrating method between a kind of ground satellite station station based on pseudo satellite, pseudolite |
| US10874372B2 (en) | 2016-02-22 | 2020-12-29 | Shanghai United Imaging Healthcare Co., Ltd. | Systems and methods for controlling an X-ray tube filament |
| WO2021194864A1 (en) * | 2020-03-23 | 2021-09-30 | Caterpillar Inc. | Software-based time rollover detection |
-
2010
- 2010-04-19 CN CN 201020167086 patent/CN201654495U/en not_active Expired - Lifetime
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102221816A (en) * | 2010-04-19 | 2011-10-19 | 普天信息技术研究院有限公司 | Satellite time serving all-in-one machine and time serving method thereof |
| CN102221816B (en) * | 2010-04-19 | 2013-01-30 | 普天信息技术研究院有限公司 | Satellite time service integrated machine and its time service method |
| CN102035607A (en) * | 2010-12-08 | 2011-04-27 | 大唐移动通信设备有限公司 | Method and device for sending calibration data |
| CN102035607B (en) * | 2010-12-08 | 2013-04-03 | 大唐移动通信设备有限公司 | Method and device for sending calibration data |
| CN102221818A (en) * | 2011-05-24 | 2011-10-19 | 国网电力科学研究院 | Transmission method for converting pulse time signals into differential bus signals by GPS (global positioning system) |
| CN105589328A (en) * | 2014-10-22 | 2016-05-18 | 中国移动通信集团公司 | Time synchronization test method and apparatus, and time synchronization testing precision determination method and apparatus |
| US10874372B2 (en) | 2016-02-22 | 2020-12-29 | Shanghai United Imaging Healthcare Co., Ltd. | Systems and methods for controlling an X-ray tube filament |
| CN107070567A (en) * | 2017-04-06 | 2017-08-18 | 中国科学院国家授时中心 | Time delay calibrating method between a kind of ground satellite station station based on pseudo satellite, pseudolite |
| CN107070567B (en) * | 2017-04-06 | 2020-04-10 | 中国科学院国家授时中心 | Satellite ground station inter-station time delay calibration method based on pseudo satellite |
| WO2021194864A1 (en) * | 2020-03-23 | 2021-09-30 | Caterpillar Inc. | Software-based time rollover detection |
| US11709277B2 (en) | 2020-03-23 | 2023-07-25 | Caterpillar Inc. | Software-based time rollover detection |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201654495U (en) | Satellite timing machine | |
| CN102221816A (en) | Satellite time serving all-in-one machine and time serving method thereof | |
| CN105187275B (en) | A kind of method and device for measuring the asymmetric time delay of fiber transmission link | |
| US20070147562A1 (en) | Corrrecting time synchronization inaccuracy caused by asymmetric delay on a communication link | |
| ES2604477T3 (en) | Method and device for time synchronization | |
| KR101479483B1 (en) | Method for correcting an asymmetry in a delay | |
| US8953645B2 (en) | Communication system, communication apparatus and time synchronization method | |
| KR101290643B1 (en) | Method and system for bearing time synchronization protocol in optical transport network | |
| CN102638324B (en) | Method and device for realizing precise time synchronization | |
| CN102142891B (en) | Optical fiber length measuring method, time synchronizing method, corresponding device and system | |
| CN106506106B (en) | High-precision time frequency source based on optical fiber time transmission | |
| CN111869280B (en) | Method and device for synchronously positioning network | |
| CN101594222B (en) | Interface testing method and device | |
| CN102742190A (en) | Synchronization method, device, and system | |
| JP2010041899A (en) | Protection relay system | |
| US10018488B2 (en) | Sensor arrangement and method for creating an output signal | |
| CN102457372B (en) | Communication system and method for transmitting clock signals by using optical fiber | |
| JPWO2009118878A1 (en) | PON system | |
| CN221263816U (en) | High-precision ultra-wideband wireless clock synchronization circuit system | |
| CN106559298B (en) | High-precision synchronous data transmission method and device for Ethernet serial port cooperative vibration monitoring system | |
| CN103595588A (en) | Method for accurately measuring asynchronous Ethernet circuit time delay | |
| CN211086574U (en) | A wireless calibration device for DC transformer based on GPRS communication | |
| CN106603184A (en) | High-precision multi-station fiber time synchronization method | |
| CN108809416B (en) | A remote base station delay measurement system and method based on short optical fiber calibration | |
| CN116347586B (en) | Device and method for calibrating delay parameters of wireless ad hoc network |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: CHINA POTEVIO CO., LTD. Free format text: FORMER OWNER: PUTIAN IT TECH INST CO., LTD. Effective date: 20130918 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20130918 Address after: 100080, No. two, 2 street, Zhongguancun science and Technology Park, Beijing, Haidian District Patentee after: China Potevio Information Industry Co., Ltd. Address before: 100080 Beijing, Haidian, North Street, No. two, No. 6, No. Patentee before: Putian IT Tech Inst Co., Ltd. |
|
| ASS | Succession or assignment of patent right |
Owner name: PUTIAN IT TECH INST CO., LTD. Free format text: FORMER OWNER: CHINA POTEVIO CO., LTD. Effective date: 20131210 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20131210 Address after: 100080 Beijing, Haidian, North Street, No. two, No. 6, No. Patentee after: Putian IT Tech Inst Co., Ltd. Address before: 100080, No. two, 2 street, Zhongguancun science and Technology Park, Beijing, Haidian District Patentee before: China Potevio Information Industry Co., Ltd. |
|
| CX01 | Expiry of patent term |
Granted publication date: 20101124 |
|
| CX01 | Expiry of patent term |