CN109405673A - Intelligent missile-borne remote-measuring equipment - Google Patents
Intelligent missile-borne remote-measuring equipment Download PDFInfo
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- CN109405673A CN109405673A CN201811393817.4A CN201811393817A CN109405673A CN 109405673 A CN109405673 A CN 109405673A CN 201811393817 A CN201811393817 A CN 201811393817A CN 109405673 A CN109405673 A CN 109405673A
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- Prior art keywords
- parameter
- module
- transmission
- priority
- fault
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Selective Calling Equipment (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The invention proposes a kind of intelligent missile-borne remote-measuring equipments.This equipment includes: parameter and standard module, for storing the information of parameter judgment criteria and priority；Data processing module judges according to guided missile parameter of the parameter judgment criteria stored in parameter and standard module to acquisition；Data coding module reserves a certain number of bytes for acquiring the design parameter value of fault parameter: when whole parameters are normal, according to parameter priority transmission parameter values；When a failure occurs, transmission fault parameter first；The high parameter value of transmission priority again when there is byte surplus；After fault parameter restores normal, transmission fault parameter is being kept after a certain period of time, again according to parameter priority configured transmission；The present invention is not in the case where increasing telemetry data transmission rate, by prejudging, will be passed under the high parameter values of parameter interpretation result and fault parameter or priority.1 times or more of parameter acquisition quantity can be improved compared with conventional telemetry equipment in the equipment.
Description
Technical field
The present invention relates to remote-measuring equipment technical field more particularly to a kind of intelligent missile-borne remote-measuring equipments.
Background technique
Missile-borne remote-measuring equipment, as guided missile system becomes increasingly complex, needs to adopt for acquiring each system operational parameters of guided missile
The number of parameters of collection is more and more.It under normal circumstances, is to meet multi-parameter by improving the data transmission code rate of remote-measuring equipment
Acquisition demand.But the raising of telemetry data transmission code rate will affect remote-measuring equipment operating distance, and remote-measuring equipment is more complicated.
Summary of the invention
In consideration of it, the present invention provides a kind of intelligent missile-borne remote-measuring equipments in order to improve the number of samples of parameter.This sets
Standby includes: parameter collection module, parameter and standard module, data processing module, data coding module, data transmission module, in which:
Parameter collection module, for completing the acquisition of guided missile parameter；
Parameter and standard module, for storing the information of parameter judgment criteria and priority；
Data processing module is carried out according to guided missile parameter of the parameter judgment criteria stored in parameter and standard module to acquisition
Judgement；
Data coding module, according to data transmission code rate requirement, is reserved certain for completing the coding to guided missile parameter
The byte of quantity is used to acquire the design parameter value of fault parameter: when whole parameters are normal, being transmitted and is joined according to parameter priority
Numerical value；When a failure occurs, transmission fault parameter first；The high parameter value of transmission priority again when there is byte surplus；When event
After barrier Parameter reconstruction is normal, transmission fault parameter is being kept after a certain period of time, again according to parameter priority configured transmission；
Data transmission module, for the telemetry for completing coding to be wirelessly transferred.
Technical effect of the invention may is that in the case where not increasing telemetry data transmission rate, by adopting to guided missile
Collection parameter is prejudged, and will be passed under the high parameter values of parameter interpretation result and fault parameter or priority.This sets
It is standby compared with conventional telemetry equipment, 1 times or more of parameter acquisition quantity can be improved.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, will make below to required in the embodiment of the present invention
Attached drawing is briefly described, it is therefore apparent that drawings described below is only some embodiments of the present invention, for this
For the technical staff in field, without creative efforts, it can also be obtained according to these attached drawings other attached
Figure.
Fig. 1 is a kind of schematic diagram of intelligent missile-borne remote-measuring equipment of the present invention.
Wherein, 1 parameter collection module, 2 parameter and standard modules, 3 data processing modules, 4 data coding modules, 5 data pass
Defeated module.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described.Obviously, described embodiment is
A part of the embodiment of the present invention, rather than whole embodiments.Based on the embodiments of the present invention, those skilled in the art
Without making creative work, every other embodiment obtained, shall fall within the protection scope of the present invention.
The feature and illustrative examples of various aspects of the invention is described more fully below.In following detailed description
In, many details are proposed, in order to provide complete understanding of the present invention.But come for those skilled in the art
It says it will be apparent that the present invention can be implemented in the case where not needing some details in these details.Below to reality
The description of example is applied just for the sake of providing and better understanding to of the invention by showing example of the invention.The present invention is never
It is limited to any specific setting and method set forth below, but covering finishes under the premise of without departing from the spirit of the present invention
Structure, method, any improvement of device, substitutions and modifications.In the the accompanying drawings and the following description, well known structure and skill is not shown
Art is unnecessary fuzzy to avoid causing to the present invention.
It should be noted that in the absence of conflict, the feature in the embodiment of the present invention and embodiment can be tied mutually
It closes, each embodiment mutually can be referred to and be quoted.The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
Fig. 1 is a kind of schematic diagram of intelligent missile-borne remote-measuring equipment of one embodiment of the invention.
As shown in Figure 1, intelligent missile-borne remote-measuring equipment may include: parameter collection module 1, parameter and standard module 2, data
Processing module 3, data coding module 4, data transmission module 5.
Wherein, parameter collection module 1 can be made of signal conditioning circuit, A/D conversion circuit and signal acquisition circuit, be used
In the acquisition for completing guided missile various parameters；Parameter and standard module 2 can lead to for storing the information such as parameter judgment criteria, priority
It crosses host computer and carries out transmission setting；Data processing module 3 is completed according to the judgment criteria of parameter and standard module 2 to acquisition parameter
Judgement.
Data coding module 4 can be used for completing the coding to each parameter, each parameter using 1bit binary data into
Row coding.According to data transmission code rate requirement, a certain number of bytes are reserved for acquiring the design parameter value of fault parameter:
When whole parameters are normal, according to parameter priority transmission parameter values；When a failure occurs, transmission fault parameter first, when having
The high parameter value of transmission priority again when byte surplus；After fault parameter restores normal, one timing of transmission fault parameter is being kept
Between after, again according to parameter priority configured transmission.The telemetry that data transmission module 5 is used to complete coding carries out wireless
Transmission.
In some embodiments, parameter collection module 1, parameter and standard module 2, data processing module 3, data coding module
4, data transmission module 5 use integrated design, peripheral hardware parameter acquisition interface, parameter and standard library loading interface, power supply interface and
Antennal interface.
In some embodiments, the test method of intelligent missile-borne remote-measuring equipment may comprise steps of:
Intelligent missile-borne remote-measuring equipment is connect with host computer, parameter and standard module 2 is configured；
The acquisition of the completion guided missile various parameters of parameter collection module 1；
Data processing module 3 completes the judgement to acquisition parameter according to the judgment criteria of parameter and standard module 2；
Data coding module 4 is used to complete the coding to each parameter, according to data transmission code rate requirement, reserves a fixed number
The byte of amount is used to acquire the design parameter value of fault parameter:
When whole parameters are normal, according to parameter priority transmission parameter values；
When a failure occurs, transmission fault parameter first, the high parameter value of transmission priority again when there is byte surplus；
After fault parameter restores normal, transmission fault parameter is being kept after a certain period of time, again according to parameter priority
Configured transmission.
The data transmission module 5 is used to for the telemetry for completing coding being wirelessly transferred.
It should be noted that above-mentioned flow operations can carry out different degrees of combined application, for simplicity, repeating no more
The sequence of above-mentioned operating procedure can be carried out spirit according to actual needs by various combined implementations, those skilled in the art
Adjustment living, or above-mentioned steps are subjected to the operation such as flexible combination.
It should be noted that the implementation of functional unit shown in above-described embodiment can be hardware, software, firmware
Or their combination.When realizing in hardware, it may, for example, be electronic circuit, specific integrated circuit (ASIC), fit
When firmware, plug-in unit, function card etc..When being realized with software mode, element of the invention is used to execute required task
Program or code segment.Perhaps code segment can store in machine readable media or by carrying in carrier wave program
Data-signal is sent in transmission medium or communication links." machine readable media " may include being capable of storage or transmission information
Any medium.The example of machine readable media includes electronic circuit, semiconductor memory devices, ROM, flash memory, erasable ROM
(EROM), floppy disk, CD-ROM, CD, hard disk, fiber medium, radio frequency (RF) link, etc..Code segment can via such as because
The computer network of special net, Intranet etc. is downloaded.
Finally it should be noted that: the above embodiments are merely illustrative of the technical solutions of the present invention, but protection of the invention
Range is not limited thereto, and anyone skilled in the art in the technical scope disclosed by the present invention, can be thought easily
It is modified or replaceed to various equivalent, these, which are modified or replaceed, should all be included within the scope of the present invention.
Claims (6)
1. a kind of intelligence missile-borne remote-measuring equipment characterized by comprising
Parameter collection module (1), parameter and standard module (2), data processing module (3), data coding module (4), data transmission
Module (5), in which:
The parameter collection module (1), for completing the acquisition of guided missile parameter；
The parameter and standard module (2), for storing the information of parameter judgment criteria and priority；
The data processing module (3) is joined according to guided missile of the parameter judgment criteria stored in parameter and standard module (2) to acquisition
Number is judged；
The data coding module (4), according to data transmission code rate requirement, is reserved for completing the coding to guided missile parameter
A certain number of bytes are used to acquire the design parameter value of fault parameter:
When whole parameters are normal, according to parameter priority transmission parameter values；
When a failure occurs, transmission fault parameter first；
The high parameter value of transmission priority again when there is byte surplus；
After fault parameter restores normal, is keeping transmission fault parameter after a certain period of time, transmitted again according to parameter priority
Parameter；
The data transmission module (5), for the telemetry for completing coding to be wirelessly transferred.
2. equipment according to claim 1, which is characterized in that wherein:
The parameter collection module (1) includes: signal conditioning circuit, A/D conversion circuit and signal acquisition circuit.
3. equipment according to claim 1, which is characterized in that wherein:
The parameter and standard module (2), for carrying out the information of transmission setup parameter judgment criteria and priority by host computer.
4. equipment according to claim 1, which is characterized in that wherein:
The data coding module (4), for being encoded to each parameter using 1bit binary data.
5. equipment according to claim 1, which is characterized in that further include:
Peripheral hardware parameter acquisition interface, parameter and standard library loading interface, power supply interface and antennal interface.
6. equipment according to claim 1, which is characterized in that the test method of the equipment the following steps are included:
Intelligent missile-borne remote-measuring equipment is connect with host computer, parameter and standard module (2) is configured；
The acquisition of parameter collection module (1) completion guided missile various parameters；
Data processing module (3) completes the judgement to acquisition parameter according to the judgment criteria of parameter and standard module (2)；
Data coding module (4) is used to complete the coding to each parameter, according to data transmission code rate requirement, reserves certain amount
Byte be used to acquire the design parameter value of fault parameter:
When whole parameters are normal, according to parameter priority transmission parameter values；
When a failure occurs, transmission fault parameter first, the high parameter value of transmission priority again when there is byte surplus；
After fault parameter restores normal, is keeping transmission fault parameter after a certain period of time, transmitted again according to parameter priority
Parameter.
The data transmission module (5) is used to for the telemetry for completing coding being wirelessly transferred.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811393817.4A CN109405673B (en) | 2018-11-21 | 2018-11-21 | Intelligent missile-borne telemetering equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811393817.4A CN109405673B (en) | 2018-11-21 | 2018-11-21 | Intelligent missile-borne telemetering equipment |
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| Publication Number | Publication Date |
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| CN109405673A true CN109405673A (en) | 2019-03-01 |
| CN109405673B CN109405673B (en) | 2020-10-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201811393817.4A Active CN109405673B (en) | 2018-11-21 | 2018-11-21 | Intelligent missile-borne telemetering equipment |
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| CN102323941A (en) * | 2011-09-01 | 2012-01-18 | 北京空间飞行器总体设计部 | Telemetry data processing method |
| CN104168148A (en) * | 2014-05-04 | 2014-11-26 | 杭州立地信息技术有限公司 | Multi-interface data collecting device and method |
| US20150051873A1 (en) * | 2012-03-22 | 2015-02-19 | Mbda France | Device for the surveillance of a weapon system, particularly of missile type |
| CN105164370A (en) * | 2013-02-25 | 2015-12-16 | 开拓工程股份有限公司 | Integrated downhole system with plural telemetry subsystems |
| CN107065706A (en) * | 2017-06-13 | 2017-08-18 | 南京金水尚阳信息技术有限公司 | A kind of distributed telemetry station working-condition monitoring system |
| CN107395264A (en) * | 2017-07-19 | 2017-11-24 | 上海航天测控通信研究所 | A kind of communicator and method based on IP+over+CCSDS+AOS standards |
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2018
- 2018-11-21 CN CN201811393817.4A patent/CN109405673B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102323941A (en) * | 2011-09-01 | 2012-01-18 | 北京空间飞行器总体设计部 | Telemetry data processing method |
| US20150051873A1 (en) * | 2012-03-22 | 2015-02-19 | Mbda France | Device for the surveillance of a weapon system, particularly of missile type |
| CN105164370A (en) * | 2013-02-25 | 2015-12-16 | 开拓工程股份有限公司 | Integrated downhole system with plural telemetry subsystems |
| CN104168148A (en) * | 2014-05-04 | 2014-11-26 | 杭州立地信息技术有限公司 | Multi-interface data collecting device and method |
| CN107065706A (en) * | 2017-06-13 | 2017-08-18 | 南京金水尚阳信息技术有限公司 | A kind of distributed telemetry station working-condition monitoring system |
| CN107395264A (en) * | 2017-07-19 | 2017-11-24 | 上海航天测控通信研究所 | A kind of communicator and method based on IP+over+CCSDS+AOS standards |
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| Publication number | Publication date |
|---|---|
| CN109405673B (en) | 2020-10-16 |
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