CN105737814B - The method of ground-to-air missile systems real-time calibration - Google Patents
The method of ground-to-air missile systems real-time calibration Download PDFInfo
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- CN105737814B CN105737814B CN201410747294.4A CN201410747294A CN105737814B CN 105737814 B CN105737814 B CN 105737814B CN 201410747294 A CN201410747294 A CN 201410747294A CN 105737814 B CN105737814 B CN 105737814B
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Abstract
The method that the present invention discloses ground-to-air missile systems real-time calibration.This method will demarcate version number as the whether newer mark of nominal data, other vehicles by the calibration version number judge nominal data, and whether there is or not updates, when there is update, nominal data application order is sent out to this vehicle, this vehicle sends newer nominal data after receiving application order to other vehicles, realizes automatically completing for weapon system calibration process, the high degree of automation of weapon system calibration process, manual operation is not depended on, calibration speed is fast.
Description
Technical field
The present invention relates to air missile weapon system more particularly to the methods of ground-to-air missile systems real-time calibration.
Background technology
For the fast pace of adaptation modern war, the reaction speed for improving weapon system is needed, the combat readiness time is shortened, this
Just to the automation of Weapon system Equipment operation, more stringent requirements are proposed, some necessary operating process are preferably automatic complete
At to reduce operating personnel's burden.Weapon system calibration is the necessary condition of weapon system operation, and calibration refers to system Nei Geche
Respective positions value is measured, including longitude, latitude, height above sea level and headstock be towards angle, and informs other vehicles in system
Process, be the basis that follow-up combat data resolves.If real-time calibration and nominal data can be updated between each vehicle automatically,
The operational performance and ease for use of weapon system will be greatly improved.
Current weapon system calibration is usually used between artificial calibration, manually input nominal data and each vehicle manually more
New mode carries out.Detailed process is as follows：
The first, weapon system bicycle is voluntarily demarcated.Choose vehicle center position in the vehicle position generally demarcated.
If vehicle is equipped with positioning and directing navigation equipment, vehicle location is navigation device position, navigation equipment by satellite positioning,
Automatically determine the nominal data of vehicle.
It the second, can be by being manually entered or computer adds automatically by manually demarcating or after navigation equipment obtains nominal data
Nominal data is entered into this vehicle processing computer by the mode for carrying and confirming through manual amendment.
Third, when have vehicle carry out proving operation after, other vehicles obtain the calibration position of the vehicle by manual operation
It sets, completes the renewal process of weapon system nominal data.
Existing method is disadvantageous in that：The degree of automation of weapon system calibration process is not high, especially relies on artificial
Operation, if manipulator, without drive control, weapon system can not differentiate whether nominal data updates, and calibration process will be unable to
It completes, moreover, because the participation of human factor, calibration speed is slow.
Invention content
Problems solved by the invention is the not high problem of the degree of automation of existing weapons system calibrating process.
To solve the above problems, the present invention provides a kind of method of ground-to-air missile systems real-time calibration, this method packet
Include following steps：S1, this vehicle resolve computer and read this vehicle nominal data from navigation equipment, in the nominal data and former calibration number
When according to differing, former nominal data and former calibration version number are updated, calibration version number is the whether newer mark of nominal data；
S2, this vehicle are resolved computer and are at least sent calibration version number to other vehicles with predetermined period；S3, other vehicles will come from this vehicle
The calibration version number for resolving computer was compared with the calibration version number in upper period, when calibration version number differs, Xiang Ben
Vehicle sends out nominal data application order；S4, this vehicle resolve computer after receiving nominal data application order, are demarcated to request
The vehicle of data sends out nominal data；S5, it asks the vehicle of nominal data after the nominal data for receiving the transmission of this vehicle, will preserve
The vehicle nominal data and calibration version number be updated.
In further scheme, when the nominal data is differed with former nominal data, updates former nominal data and marked with former
Determining version number includes：This vehicle resolves computer automatic decision nominal data and former nominal data, when the two differs, automatically more
New source nominal data and former calibration version number；Alternatively, operator demarcates original after this vehicle resolves computer acquisition nominal data
Data and former calibration version number update former nominal data and former calibration version number after modifying.
In further scheme, it is to send to have mark that this vehicle, which resolves computer and at least sends calibration version number to other vehicles,
Determine the heartbeat message of version number.
In further scheme, the calibration version number is the calibration version number of a byte.
Compared with prior art, the present invention has the following advantages：
Due to that will demarcate version number as the whether newer mark of nominal data, other vehicles are sentenced by the calibration version number
Whether there is or not updates for disconnected nominal data, when there is update, send out nominal data application order to this vehicle, this vehicle is receiving application order
Newer nominal data is sent to other vehicles afterwards, realizes automatically completing for weapon system calibration process, weapon system mark
The high degree of automation for determining process, does not depend on manual operation, and calibration speed is fast.
Description of the drawings
Fig. 1 is the flow chart of the method for ground-to-air missile systems real-time calibration of the present invention.
Specific implementation mode
For technology contents, construction feature, institute's reached purpose and effect that the present invention will be described in detail, below in conjunction with embodiment
And attached drawing is coordinated to be described in detail.
Referring to Fig. 1, the method for ground-to-air missile systems real-time calibration of the present invention includes the following steps：
S1, this vehicle resolve computer and read this vehicle nominal data from navigation equipment, in the nominal data and former nominal data
When differing, former nominal data and former calibration version number are updated, calibration version number is the whether newer mark of nominal data.At this
In step, how to judge that nominal data is differed with former nominal data and prior art may be used.In this step, the former mark of update
There are many modes for fixed number evidence and former calibration version number, for example, this vehicle resolves computer automatic decision nominal data and former calibration number
According to when the two differs, automatically updating former nominal data and former calibration version number；It is calculated alternatively, operator resolves in this vehicle
After machine obtains nominal data, former nominal data and former calibration are updated to former nominal data and former demarcate after version number modifies
Version number.In this step, calibration version number adds up after demarcating every time, as the updated label of calibration.Demarcating version number can
With using the representation method in mature technology, for example, nominal data 1, nominal data 2, nominal data 2 is indicated to nominal data 1
Nominal data after being updated.
S2, this vehicle are resolved computer and are at least sent calibration version number to other vehicles with predetermined period.In the skill of the present invention
Art design in, be by demarcate version number to judge nominal data, whether there is or not updates, so, at least need send calibration version number.
In the present embodiment, it is to send the heartbeat message with calibration version number.In the present embodiment, it is contemplated that nominal data
Data volume is larger, and the nominal data update frequency is extremely low, and each cycle is all sent out and can be caused stress to communication system, therefore only sends 1
The calibration version number of byte.
S3, other vehicles will resolve the calibration version number of computer from this vehicle and the calibration version number in upper period compares
Compared with, demarcate version number differ when, send out nominal data application order to this vehicle；In this step, calibration version number with it is upper
Period differs, and shows that the nominal data of this vehicle has been updated.
S4, this vehicle resolve computer after receiving nominal data application order, are sent out to the vehicle of request nominal data
Nominal data.
S5, ask the vehicle of nominal data after the nominal data for receiving the transmission of this vehicle, by the vehicle nominal data of preservation
Version number is updated with calibration, one of the input as data calculation.So far the calibration process of entire weapon system is completed.
In conclusion the method for ground-to-air missile systems real-time calibration of the present invention will demarcate version number as nominal data
Whether newer mark, other vehicles by the calibration version number judge nominal data, and whether there is or not updates, when there is update, Xiang Benche
Nominal data application order is sent out, this vehicle sends newer nominal data to other vehicles after receiving application order, realizes
The automatically completing of weapon system calibration process.After bicycle updates nominal data, the other each vehicles of weapon system automatically update this
Vehicle nominal data, without manual operation.Reduce influence of the manual operation to calibration process to the greatest extent, has accomplished in real time
Calibration.It is verified through l-G simulation test, the present invention can greatly improve the calibration speed of weapon system, disregard handling time and communication
In the case of time, entire renewal process no more than 3 of demarcating resolves the period.Applicability is wide, and it is military to can be used for various distributed interactive
Device system.
Claims (4)
1. the method for ground-to-air missile systems real-time calibration, it is characterized in that：This method comprises the following steps：
S1, this vehicle resolve computer and read this vehicle nominal data from navigation equipment, in the nominal data and original nominal data not phase
Meanwhile former nominal data and former calibration version number are updated, calibration version number is the whether newer mark of nominal data；
S2, this vehicle are resolved computer and are at least sent calibration version number to other vehicles with predetermined period；
The calibration version number that computer is resolved from this vehicle was compared by S3, other vehicles with the calibration version number in upper period,
When calibration version number differs, nominal data application order is sent out to this vehicle；
S4, this vehicle resolve computer after receiving nominal data application order, and calibration is sent out to the vehicle of request nominal data
Data；
S5, ask the vehicle of nominal data after the nominal data for receiving the transmission of this vehicle, by the vehicle nominal data and mark of preservation
Determine version number to be updated.
2. the method for ground-to-air missile systems real-time calibration as described in claim 1, it is characterized in that：In the nominal data and original
When nominal data differs, updates former nominal data and former calibration version number includes：This vehicle resolves the calibration of computer automatic decision
Data and former nominal data automatically update source nominal data and former calibration version number when the two differs；Alternatively, operator
After this vehicle resolves computer acquisition nominal data, original mark is updated after modifying to former nominal data and former calibration version number
Fixed number evidence and former calibration version number.
3. the method for ground-to-air missile systems real-time calibration as described in claim 1, it is characterized in that：This vehicle resolve computer to
It is to send the heartbeat message with calibration version number that other vehicles, which at least send calibration version number,.
4. the method for ground-to-air missile systems real-time calibration as claimed in claim 3, it is characterized in that：The calibration version number is
The calibration version number of one byte.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410747294.4A CN105737814B (en) | 2014-12-10 | 2014-12-10 | The method of ground-to-air missile systems real-time calibration |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410747294.4A CN105737814B (en) | 2014-12-10 | 2014-12-10 | The method of ground-to-air missile systems real-time calibration |
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| Publication Number | Publication Date |
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| CN105737814A CN105737814A (en) | 2016-07-06 |
| CN105737814B true CN105737814B (en) | 2018-08-03 |
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| CN201410747294.4A Active CN105737814B (en) | 2014-12-10 | 2014-12-10 | The method of ground-to-air missile systems real-time calibration |
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Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113778046B (en) * | 2021-02-25 | 2023-09-01 | 京东鲲鹏(江苏)科技有限公司 | Calibration data and calibration model updating method and device of chassis of drivable equipment |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1265495A (en) * | 1998-12-23 | 2000-09-06 | 电脑相关想象公司 | Method and device for enabling accession of automatic acknowledge service unit for foreign country system |
| CN1288199A (en) * | 1999-09-09 | 2001-03-21 | 日本电气株式会社 | Method for updating customer's mounting data respons costomer raising events |
| CN101127960A (en) * | 2007-09-20 | 2008-02-20 | 中兴通讯股份有限公司 | A system and method for differential update of electronic service guidance |
| CN102339453A (en) * | 2011-10-17 | 2012-02-01 | 天泽信息产业股份有限公司 | Vehicle position sharing system and implementation method thereof |
-
2014
- 2014-12-10 CN CN201410747294.4A patent/CN105737814B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1265495A (en) * | 1998-12-23 | 2000-09-06 | 电脑相关想象公司 | Method and device for enabling accession of automatic acknowledge service unit for foreign country system |
| CN1288199A (en) * | 1999-09-09 | 2001-03-21 | 日本电气株式会社 | Method for updating customer's mounting data respons costomer raising events |
| CN101127960A (en) * | 2007-09-20 | 2008-02-20 | 中兴通讯股份有限公司 | A system and method for differential update of electronic service guidance |
| CN102339453A (en) * | 2011-10-17 | 2012-02-01 | 天泽信息产业股份有限公司 | Vehicle position sharing system and implementation method thereof |
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| CN105737814A (en) | 2016-07-06 |
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