CN109388852A - A kind of rocket bomb transmitting number accurate metering method - Google Patents
A kind of rocket bomb transmitting number accurate metering method Download PDFInfo
- Publication number
- CN109388852A CN109388852A CN201811044008.2A CN201811044008A CN109388852A CN 109388852 A CN109388852 A CN 109388852A CN 201811044008 A CN201811044008 A CN 201811044008A CN 109388852 A CN109388852 A CN 109388852A
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- China
- Prior art keywords
- rocket
- bomb transmitting
- projectile
- value
- rocket bomb
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
-
- 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
- F42B35/02—Gauging, sorting, trimming or shortening cartridges or missiles
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/30—Computing systems specially adapted for manufacturing
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- Computer Hardware Design (AREA)
- Evolutionary Computation (AREA)
- Geometry (AREA)
- General Physics & Mathematics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention discloses a kind of rocket bomb transmitting number accurate metering method, can carry out accurate metering to bullet number during rocket bomb transmitting.By counting to the detection of rocket bomb transmitting apparatus overload amount to the bullet number during rocket bomb transmitting, the accurate metering to rocket bomb transmitting number is realized.Specifically: before the igniting of in-orbit rocket projectile, the overload quantity of rocket bomb transmitting equipment is measured, if overload quantity is less than setting value, it is believed that do not launch a rocket shell at this time；After to the igniting of in-orbit rocket projectile, rocket bomb transmitting apparatus overload amount is measured again at the setting moment, when measured value is greater than the set value, it is believed that the acceleration for emitting it is applied with to rocket projectile；Finally behind setting time interval, rocket bomb transmitting apparatus overload amount is measured again, if overload quantity is less than setting value, then it is assumed that rocket bomb transmitting success.
Description
Technical field
The present invention relates to a kind of method of counting, and in particular to a kind of rocket projectile hair number penetrates method of counting.
Background technique
When weather modification anti-hail operation, catalyst is sent into cloud layer by the way of launching a rocket shell, thus
Realize the function of anti-hail.When operation, the quantity of the rocket projectile emitted is affected to operation quality, and due to rocket
Bullet belongs to priming system, need to must record in real time to the stringent control of its quantity, the bullet number of each setting operation.
Summary of the invention
In view of this, the present invention provides a kind of rocket bomb transmitting number accurate metering method, it can be in rocket bomb transmitting process
In to bullet number carry out accurate metering.
The rocket bomb transmitting number accurate metering method, specifically: pass through the inspection to rocket bomb transmitting apparatus overload amount
It surveys to be counted to the bullet number during rocket bomb transmitting, specifically:
Before the igniting of in-orbit rocket projectile, the overload quantity of rocket bomb transmitting equipment is measured, enabling measured value is W, when W is less than setting
When value D, it is believed that do not launch a rocket shell at this time；
Enabling the rocket projectile igniting time started is t1, and the igniting end time is t2；After to the igniting of in-orbit rocket projectile, in t3
It carves and measures rocket bomb transmitting apparatus overload amount again, enabling measured value is V, and setting time interval is met between t1 and t3；When V is greater than
When setting value E, it is believed that be applied with the acceleration for emitting it to rocket projectile；
Behind setting time interval, rocket bomb transmitting apparatus overload amount is measured again at the t4 moment, if t4 moment overload quantity is small
In setting value D, then it is assumed that rocket bomb transmitting success；1 then is added to rocket bomb transmitting number.
Further include surveying resistance detection:
Before the igniting of in-orbit rocket projectile, track resistance value first where measurement rocket projectile, enabling surveyed resistance value is X, when X is being set
Standard resistance range (A, B) it is interior when, it is believed that rocket projectile is in-orbit, into next step；Otherwise it is assumed that there is no rocket projectile on track；
After to the igniting of in-orbit rocket projectile, track resistance value is measured again, enabling surveyed resistance value is Y, when Y is greater than the set value C,
Think rocket bomb transmitting success；
When the testing result of the rocket bomb transmitting apparatus overload amount and the testing result for surveying resistance detection are " rocket
Play successful launch " when, 1 is added to rocket bomb transmitting number.
3, rocket bomb transmitting number accurate metering method as claimed in claim 1 or 2, it is characterised in that: between t1 and t3
Meet: 5ms < t3-t1 < 50ms；Meet between t3 and t4: t4-t3 < 3S.
The utility model has the advantages that
(1) when realizing rocket launching by pulse firing mode, rocket launching process is judged by the variation of overload quantity,
Judge whether to meet autogenous ignition condition by pulse firing and the variation of overload quantity timing, to realize to rocket bomb transmitting number
Accurate metering excludes artificial the case where faking.
(2) surveying to hinder to detect to match with overload quantity detection can be further ensured that the accurate of rocket bomb transmitting counting number
Property.
Detailed description of the invention
Fig. 1 is rocket-firing system firing pulse schematic diagram；
Fig. 2 is rocket-firing system overload quantity absolute value schematic diagram.
Specific embodiment
With reference to the accompanying drawings and examples, the present invention is described in further detail.
The present embodiment provides one kind during increasing rain artificially with hail suppression, is accurately counted to the rocket projectile emitted
Several technical methods.
This method specifically includes survey resistance detection and overload quantity detects two parts.
One, resistance detection is surveyed
1.1 measure rocket projectile place track resistance value by AD Acquisition Circuit, and enabling surveyed resistance value is X, when X is in the resistance value of setting
In range (A, B), that is, when meeting A < X < B, it is believed that rocket projectile is in-orbit, into next step；Otherwise it is assumed that there is no rocket on track
Bullet；
1.2 give the firing pulse of one 200ms of rocket projectile, light a fire to in-orbit rocket projectile；Rocket projectile is enabled to light a fire the time started
For t1, the igniting end time is t2, and interval is about 200ms between t1 and t2；As shown in Figure 1；
After 1.3 igniting, track resistance value is measured again, and enabling surveyed resistance value is Y, when Y is greater than the set value C, that is, meets Y > C
When, it is believed that rocket projectile derails (successful launch).
Two, overload quantity detects
The overload quantity (amount of acceleration) of measurement rocket bomb transmitting equipment before 2.1 igniting, enabling measured value is W, when W is less than setting
When value D, i.e. W < D, it is believed that do not launch a rocket shell at this time；
2.2 measure rocket bomb transmitting apparatus overload amount after to the igniting of in-orbit rocket projectile, at the t3 moment again, t1 and t3 it
Between meet 5ms<t3-t1<50ms, as shown in Fig. 2, enable t3 moment measured value be V, when V is greater than the set value E, i.e. V>E, it is believed that
There is an acceleration to make its transmitting rocket projectile；
2.3 measure rocket bomb transmitting apparatus overload amount at the t4 moment again, and t4-t3 < 3S, such as Fig. 2 are met between t3 and t4
It is shown, if t4 moment overload quantity becomes smaller and is less than setting value D, then it is assumed that rocket projectile derails (successful launch).
When the judging result by above-mentioned survey resistance detection and overload quantity detection is " rocket projectile derails (successful launch) ",
1 is added to rocket bomb transmitting number, that is, thinks to transmit a rocket projectile, thus, it is possible to the quantity to the rocket projectile emitted to carry out essence
Really count.
To sum up, the above is merely preferred embodiments of the present invention, it is not intended to limit the scope of the present invention.It is all
Within the spirit and principles in the present invention, any modification, equivalent replacement, improvement and so on should be included in protection of the invention
Within the scope of.
Claims (3)
1. a kind of rocket bomb transmitting number accurate metering method, it is characterised in that: pass through the inspection to rocket bomb transmitting apparatus overload amount
It surveys to be counted to the bullet number during rocket bomb transmitting, specifically:
Before the igniting of in-orbit rocket projectile, the overload quantity of rocket bomb transmitting equipment is measured, enabling measured value is W, when W is less than setting value D
When, it is believed that it does not launch a rocket shell at this time；
Enabling the rocket projectile igniting time started is t1, and the igniting end time is t2；To in-orbit rocket projectile igniting after, the t3 moment again
Secondary measurement rocket bomb transmitting apparatus overload amount, enabling measured value is V, and setting time interval is met between t1 and t3；When V is greater than setting
When value E, it is believed that be applied with the acceleration for emitting it to rocket projectile；
Behind setting time interval, rocket bomb transmitting apparatus overload amount is measured again at the t4 moment, is set if t4 moment overload quantity is less than
Definite value D, then it is assumed that rocket bomb transmitting success；1 then is added to rocket bomb transmitting number.
2. rocket bomb transmitting number accurate metering method as described in claim 1, it is characterised in that: further include surveying resistance detection:
Before the igniting of in-orbit rocket projectile, track resistance value first where measurement rocket projectile, enabling surveyed resistance value is X, when X is in the resistance of setting
When value range (A, B) is interior, it is believed that rocket projectile is in-orbit, into next step；Otherwise it is assumed that there is no rocket projectile on track；
After to the igniting of in-orbit rocket projectile, track resistance value is measured again, and enabling surveyed resistance value is Y, when Y is greater than the set value C, it is believed that
Rocket bomb transmitting success；
When the testing result of the rocket bomb transmitting apparatus overload amount and the testing result for surveying resistance detection are " rocket projectile hair
Penetrate success " when, 1 is added to rocket bomb transmitting number.
3. rocket bomb transmitting number accurate metering method as claimed in claim 1 or 2, it is characterised in that: meet between t1 and t3:
5ms<t3-t1<50ms；Meet between t3 and t4: t4-t3 < 3S.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811044008.2A CN109388852B (en) | 2018-09-07 | 2018-09-07 | Rocket projectile firing number accurate counting method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811044008.2A CN109388852B (en) | 2018-09-07 | 2018-09-07 | Rocket projectile firing number accurate counting method |
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| Publication Number | Publication Date |
|---|---|
| CN109388852A true CN109388852A (en) | 2019-02-26 |
| CN109388852B CN109388852B (en) | 2023-07-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811044008.2A Active CN109388852B (en) | 2018-09-07 | 2018-09-07 | Rocket projectile firing number accurate counting method |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109855482A (en) * | 2019-03-05 | 2019-06-07 | 北京星际荣耀空间科技有限公司 | The method of discrimination and discriminating gear of Solid Launch Vehicle lift-off zero,take-off zero |
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| WO2000012953A1 (en) * | 1998-08-28 | 2000-03-09 | Royal Ordnance Plc | Ammunition safety and arming unit |
| US6332400B1 (en) * | 2000-01-24 | 2001-12-25 | The United States Of America As Represented By The Secretary Of The Navy | Initiating device for use with telemetry systems |
| CN101118140A (en) * | 2007-08-30 | 2008-02-06 | 济南卓信智能科技有限公司 | Rocket bomb transmitting counting device and counting method thereof thereof |
| JP2008175526A (en) * | 2008-03-18 | 2008-07-31 | Hitachi Kokusai Electric Inc | Device for measuring number of shot bullets |
| CN102221309A (en) * | 2011-05-20 | 2011-10-19 | 陕西中天火箭技术有限责任公司 | Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method |
| CN104567547A (en) * | 2015-01-08 | 2015-04-29 | 成都信息工程学院 | Operating data acquiring system and data processing method for silhouette rocket |
| CN204831015U (en) * | 2015-06-26 | 2015-12-02 | 罗俊颉 | Precipitation of hail of rockets emitter operation information acquisition device and system |
| CN106969667A (en) * | 2017-05-10 | 2017-07-21 | 成都信息工程大学 | A kind of shadow rocket meticulous process intelligent acquisition device and data processing method |
-
2018
- 2018-09-07 CN CN201811044008.2A patent/CN109388852B/en active Active
Patent Citations (8)
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|---|---|---|---|---|
| WO2000012953A1 (en) * | 1998-08-28 | 2000-03-09 | Royal Ordnance Plc | Ammunition safety and arming unit |
| US6332400B1 (en) * | 2000-01-24 | 2001-12-25 | The United States Of America As Represented By The Secretary Of The Navy | Initiating device for use with telemetry systems |
| CN101118140A (en) * | 2007-08-30 | 2008-02-06 | 济南卓信智能科技有限公司 | Rocket bomb transmitting counting device and counting method thereof thereof |
| JP2008175526A (en) * | 2008-03-18 | 2008-07-31 | Hitachi Kokusai Electric Inc | Device for measuring number of shot bullets |
| CN102221309A (en) * | 2011-05-20 | 2011-10-19 | 陕西中天火箭技术有限责任公司 | Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method |
| CN104567547A (en) * | 2015-01-08 | 2015-04-29 | 成都信息工程学院 | Operating data acquiring system and data processing method for silhouette rocket |
| CN204831015U (en) * | 2015-06-26 | 2015-12-02 | 罗俊颉 | Precipitation of hail of rockets emitter operation information acquisition device and system |
| CN106969667A (en) * | 2017-05-10 | 2017-07-21 | 成都信息工程大学 | A kind of shadow rocket meticulous process intelligent acquisition device and data processing method |
Non-Patent Citations (1)
| Title |
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| 辛腾达等: "某型火箭发射装置检测系统设计与实现", 《航空兵器》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109855482A (en) * | 2019-03-05 | 2019-06-07 | 北京星际荣耀空间科技有限公司 | The method of discrimination and discriminating gear of Solid Launch Vehicle lift-off zero,take-off zero |
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| CN109388852B (en) | 2023-07-28 |
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