CN106091810B - A kind of four-way MISSILE LAUNCHING time-series rules module - Google Patents
A kind of four-way MISSILE LAUNCHING time-series rules module Download PDFInfo
- Publication number
- CN106091810B CN106091810B CN201610391624.XA CN201610391624A CN106091810B CN 106091810 B CN106091810 B CN 106091810B CN 201610391624 A CN201610391624 A CN 201610391624A CN 106091810 B CN106091810 B CN 106091810B
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- Prior art keywords
- module
- way
- missile launching
- series rules
- housing
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A35/00—Accessories or details not otherwise provided for
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
Abstract
The present invention discloses a kind of four-way MISSILE LAUNCHING time-series rules module, MISSILE LAUNCHING sequential that can be simultaneously to four passages is detected, testing result is externally forwarded by CAN, while according to the MISSILE LAUNCHING sequential of respective channel, guided missile springing signal is provided in real time.The four-way MISSILE LAUNCHING time-series rules module is used as master controller, including four transmitted in both directions devices, DC/DC devices, ferroelectric memorys, CAN driving elements, electromagnetic relay member device and functional circuit using TMS320F28335 DSP.Rectangular connector of the present invention and modular structure, compared to prior art, vibration resistance and thermal diffusivity are stronger, and maintainability, protection are more preferable.
Description
Technical field
The present invention relates to ground launch control technology field, more particularly to a kind of four-way MISSILE LAUNCHING time-series rules mould
Block.
Background technology
Transmitting sequential be judge guided missile whether the critical data of normal transmission.It is launching control system weight to launch time sequence detecting circuit
Want part, performing " transmitting make " since launching control system starts, to " missile takeoff " after terminate, to launching the confession of flow Zhong Ge roads
Electricity, priming system igniting and firing box（Cylinder）The state for electrically returning announcement with guided missile is detected, and then testing result formation is sent out
Sequential is penetrated to be preserved.
The transmitting time-series rules functional circuit of current launching control system is typically coupling in one with transmitting flow perform function circuit
Rise, using identical benchmark job power supply, controlled by same controller, collectively constituted the repertoire of launching control system.Hair
Penetrate time sequence detecting circuit and exception once occur（Such as detect short circuit or disturbed by external signal）, frequently can lead to other work(
Energy circuit operation irregularity, or even occur that director demon runs " deadlock " phenomenon.In addition, controller was performed in transmitting flow
Once there is exception in journey, transmitting time series data is caused not collect, technical problem analysis afterwards will be extremely difficult.
The content of the invention
The present invention sends out to solve currently to launch caused by time sequence detecting circuit is coupled with the other functional circuits of launching control system
Control system work basic reliability reduction problem is there is provided a kind of four-way MISSILE LAUNCHING time-series rules module, by transmitting sequential inspection
Slowdown monitoring circuit is independent, on the premise of launching control system work basic reliability is not influenceed, completes MISSILE LAUNCHING time-series rules work(
Energy.
In order to reach above-mentioned purpose, the technical scheme is that providing a kind of four-way MISSILE LAUNCHING time-series rules mould
Block, wherein comprising being arranged in a housing：Master controller and the ferroelectric memory being connected respectively with the master controller, DC/
DC change-over circuits, springing output control circuit, CAN driving change-over circuits and four transmitted in both directions devices；Each transmitted in both directions device
Part is acquired to the 16 tunnels transmitting clock signal of a corresponding execution passage；Detection module is inserted by the housing
Into the pedestal matched with the housing.
Preferably, socket piece of the front side of the hull outside provided with rectangular electric connector is described to insert as output interface
Seat piece carries guide finger；Plug piece of the patch bay of the pedestal provided with rectangular electric connector is used as the defeated of follow-up component
Incoming interface, the plug piece carries guide sleeve；When inserting detection module in pedestal, the socket piece with guide finger is led with carrying
It is engaged to the plug piece of set, guiding is provided for grafting electric connector.
Preferably, the both sides up and down of the hull outside are correspondingly arranged upper rail groove and lower guideway groove, with the pedestal
The upper rail and lower guideway that both sides are set above and below inside are respectively cooperating with, and guiding is provided to insert detection module in pedestal.
Preferably, the rear side of the housing, can be in detection provided with rivet coating nut and equipped with corresponding captive screw
Module is plugged together to be fastened to the detection module afterwards in place.
Preferably, the rear side of the housing is provided with handle, and impetus is provided for module plug.
Preferably, at detection bottom of the inside of the housing provided with the CPU board containing master controller and the device containing transmitted in both directions
Plate；By brass hexagonal spacer, detection bottom plate is anchored on the inner surface of the housing, and stacks CPU board it is arranged in this
Detect on bottom plate, and ensure distance spaced between CPU board and detection bottom plate；The DC/DC change-over circuits are set
Module, is connected to the other positions that case inside surface is not connected with detection bottom plate in addition.
Preferably, the master controller uses TMS320F28335 dsp chip.
Preferably, the transmitted in both directions device uses 74ALVC164245 acquisition chips.
Preferably, the detection module is used for ground missile arm discharge system or warship face missile armament emission system.
Compared with prior art, four-way MISSILE LAUNCHING time-series rules module of the present invention, with advantages below：
1st, other functional circuits with launching control system are completely isolated, neither influence other functional circuit normal works, and not
Influenceed by other functional circuits, enhance the basic reliability of launching control system.
2nd, possess while completing four passages, the transmitting clock signal acquisition function on each tunnel of passage 16 can be by sequential
Testing result is preserved, and can be by CAN in real time by time-series rules result outgoing, with can adapt to current main-stream（Warship）
Face armament systems transmitting time-series rules demand.
3rd, guide groove is processed on module housing, guide rail is processed on the pedestal for installing module, provides and leads for module plug
To, blind plugging function is realized, it is easy to operate.
4th, the output interface of module, a band guiding are used as using the socket piece of a rectangular electric connector with guide finger
The plug piece of the rectangular electric connector of set and spring assembly can evade connector folder dead as the input interface of follow-up component
Risk, high vibration, impact complex environment in, it is ensured that the signal continuity and high reliability of connector.
Brief description of the drawings
Fig. 1 is a kind of circuit theory diagrams of four-way MISSILE LAUNCHING time-series rules module of the invention.
Fig. 2, Fig. 3 are the threedimensional models in former and later two directions outside a kind of four-way MISSILE LAUNCHING time-series rules mould of the invention
Figure.
Fig. 4 is the three-dimensional model diagram inside a kind of four-way MISSILE LAUNCHING time-series rules mould of the invention.
Fig. 5 is a kind of scheme of installation of four-way MISSILE LAUNCHING time-series rules module of the invention.
Embodiment
To describe technology contents, construction feature, institute's reached purpose and effect of the present invention in detail, given below in conjunction with accompanying drawing
To describe in detail.
Refer to shown in Fig. 1, four-way MISSILE LAUNCHING time-series rules module proposed by the present invention（Detect below or referred to as
Module）, using TMS320F28335 DSP（Digital Signal Processing）Chip is provided with four be attached thereto as master controller 11
Individual transmitted in both directions device 12, ferroelectric memory 13, DC/DC change-over circuits 14, springing output control circuit 15, CAN driving conversions
Circuit 16.
Possess four execution passages, each 16 tunnels transmitting clock signal for performing passage, by corresponding with the execution passage
A transmitted in both directions device 12 be acquired.DSP logic level is 3.3V, and outside acquisition chip is 5V operating voltages.This
Transmitted in both directions device 12 in example uses 74ALVC164245 chips, had both solved the problems, such as the voltage matches of signal acquisition, and had also subtracted
Circuit scale and number of chips are lacked, low in energy consumption, highly versatile.Using ferroelectric memory 13, realize and transmitting timing results are entered
The function of row memory storage.
Refer to shown in Fig. 2, Fig. 3, the external structure of the housing 20 of detection module of the present invention is shown, the housing 20
Both sides are correspondingly arranged on upper rail groove 21 and lower guideway groove 22 up and down, can distinguish with the upper rail set by pedestal and lower guideway
Coordinate, guiding is provided to insert detection module on pedestal.The rear side of housing 20 is provided with several rivet coating nuts 23 and each autogamy
Standby captive screw, can plug together in detection module and the module is fastened afterwards in place；The rear side of housing 20 is additionally provided with handle
24, provide impetus for module plug.The front side of housing 20 is provided with the socket piece 25 of rectangular electric connector, and guide finger is carried above
26, provide guiding for grafting electric connector.
Refer to shown in Fig. 4, inside the housing 20 of detection module, by several brass hexagonal spacers 34, will set
Transmitted in both directions device（And ferroelectric memory, springing output control circuit, CAN drive the parts such as change-over circuit）Detection bottom plate
32 are anchored on the inner surface of housing 20 of detection module, and provide installation position for the CPU board 31 for being provided with master controller
Put, stack CPU board 31 and be arranged in spaced distance on detection bottom plate 32 and between detection bottom plate 32；DC/ is set
The module 33 of DC change-over circuits is connected to the other positions of the inner surface of housing 20 in addition.
Refer to shown in Fig. 5, the pedestal 40 for inserting detection module, provided with patch bay 41；About pedestal 40
The inner surface of both sides is correspondingly arranged on upper rail and lower guideway 42, upper rail groove and lower guideway that can be with detection module housing 20
Groove is engaged, and guiding is provided for inserting module.Patch bay 41 is provided with multiple installation sites, wherein at least one installation position
The plug piece 43 of rectangular electric connector is installed, the plug piece 43 of the rectangular electric connector carries guide sleeve 44；Other installation positions
Put and can be used to set other detection modules or other functional modules of launching control system are set.
When detection module inserting is into pedestal 40, the socket piece 25 of rectangular electric connector on detection module housing 20 can
The plug piece 43 of rectangular electric connector with being installed on patch bay 41 is engaged, and the guide finger 26 and plug of socket piece 25
The guide sleeve 44 of part 43 is engaged, and guiding is provided for grafting electric connector, so as to realize blind plugging function.Guide sleeve 44 is provided with bullet
Spring component.
Wherein, the socket piece 25 of the rectangular electric connector with guide finger 26 is used as the output interface of module, band guide sleeve 44
Plug piece 43 with the rectangular electric connector of spring assembly enhances the vibration resistance of equipment as the input interface of follow-up component
And thermal diffusivity, improve maintainability, the protection level of equipment.
In summary, the present invention carries out modularized design to MISSILE LAUNCHING time sequence detecting circuit, using independent work base
Quasi- power supply, independent controller, suitable for ground（Warship）Face missile armament emission system, can complete the hair of the guided missile to four passages
Penetrate time-series rules function.Detection module housing uses boxlike dongle configuration, using being oriented to finger setting, it is possible to achieve blindmate and anti-error
Insert.
Although present disclosure is discussed in detail by above preferred embodiment, but it should be appreciated that above-mentioned
Description is not considered as limitation of the present invention.After those skilled in the art have read the above, for the present invention's
A variety of modifications and substitutions all will be apparent.Therefore, protection scope of the present invention should be limited to the appended claims.
Claims (9)
1. a kind of four-way MISSILE LAUNCHING time-series rules module, it is characterised in that comprising being arranged in a housing：Main control
Device and the ferroelectric memory being connected respectively with the master controller, DC/DC change-over circuits, springing output control circuit, CAN drivings turn
Change circuit and four transmitted in both directions devices；When each transmitted in both directions device is launched 16 tunnels of a corresponding execution passage
Sequential signal is acquired；Detection module is inserted into the pedestal matched with the housing by the housing.
2. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
Socket piece of the front side of the hull outside provided with rectangular electric connector is as output interface, and the socket piece is with guiding
Pin；The patch bay of the pedestal is provided with the plug piece of rectangular electric connector as the input interface of follow-up component, described
Plug piece carries guide sleeve；When inserting detection module in pedestal, the socket piece with guide finger and the plug with guide sleeve
Part is engaged, and guiding is provided for grafting rectangular electric connector.
3. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1 or 2, it is characterised in that
Both sides above and below the upper rail groove and lower guideway groove, with the base interior that the both sides up and down of the hull outside are correspondingly arranged
The upper rail and lower guideway of setting are respectively cooperating with, and guiding is provided to insert detection module in pedestal.
4. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The rear side of the housing can be plugged together in place provided with rivet coating nut and equipped with corresponding captive screw in detection module
The detection module is fastened afterwards.
5. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The rear side of the housing is provided with handle, and impetus is provided for module plug.
6. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
In detection bottom plate of the inside of the housing provided with the CPU board containing master controller and the device containing transmitted in both directions；Pass through brass
Hexagonal spacer, will detection bottom plate be anchored on the inner surface of the housing, and make CPU board stack be arranged in the detection bottom plate it
On, and ensure distance spaced between CPU board and detection bottom plate；The module of the DC/DC change-over circuits is set, connected in addition
It is connected on the other positions that case inside surface is not connected with detection bottom plate.
7. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The master controller uses TMS320F28335 dsp chip.
8. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The transmitted in both directions device uses 74ALVC164245 acquisition chips.
9. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The detection module is used for ground missile arm discharge system or warship face missile armament emission system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610391624.XA CN106091810B (en) | 2016-06-06 | 2016-06-06 | A kind of four-way MISSILE LAUNCHING time-series rules module |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610391624.XA CN106091810B (en) | 2016-06-06 | 2016-06-06 | A kind of four-way MISSILE LAUNCHING time-series rules module |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106091810A CN106091810A (en) | 2016-11-09 |
| CN106091810B true CN106091810B (en) | 2017-10-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610391624.XA Active CN106091810B (en) | 2016-06-06 | 2016-06-06 | A kind of four-way MISSILE LAUNCHING time-series rules module |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111312006A (en) * | 2020-03-03 | 2020-06-19 | 上海机电工程研究所 | Teaching demonstration device and method for mixed loading and launching control of multiple weapons |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114268582B (en) * | 2021-11-24 | 2024-04-05 | 上海机电工程研究所 | Bullet forwarding system and device |
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| US4293949A (en) * | 1979-10-30 | 1981-10-06 | The United States Of America As Represented By The Secretary Of The Navy | Clock invariant synchronization for random binary sequences |
| CN102809937A (en) * | 2012-08-17 | 2012-12-05 | 上海航天测控通信研究所 | PLC and 1553B based portable equivalent device for carrier rocket test-launch control system |
| CN103122807A (en) * | 2013-01-16 | 2013-05-29 | 西北工业大学 | Multichannel solid rocket engine ignition sequence control method |
| CN103558838A (en) * | 2013-11-01 | 2014-02-05 | 北京航空航天大学 | Solid-liquid power air vehicle ground test and launch control system of 422 bus |
| CN204807973U (en) * | 2015-01-22 | 2015-11-25 | 程义 | A rocket gun follow -up signal and an accuse chronogenesis detector |
| CN105572481A (en) * | 2015-12-25 | 2016-05-11 | 哈尔滨工业大学 | Guided ammunition multipath sequential state signal measuring circuit and measuring method |
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2016
- 2016-06-06 CN CN201610391624.XA patent/CN106091810B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4293949A (en) * | 1979-10-30 | 1981-10-06 | The United States Of America As Represented By The Secretary Of The Navy | Clock invariant synchronization for random binary sequences |
| CN102809937A (en) * | 2012-08-17 | 2012-12-05 | 上海航天测控通信研究所 | PLC and 1553B based portable equivalent device for carrier rocket test-launch control system |
| CN103122807A (en) * | 2013-01-16 | 2013-05-29 | 西北工业大学 | Multichannel solid rocket engine ignition sequence control method |
| CN103558838A (en) * | 2013-11-01 | 2014-02-05 | 北京航空航天大学 | Solid-liquid power air vehicle ground test and launch control system of 422 bus |
| CN204807973U (en) * | 2015-01-22 | 2015-11-25 | 程义 | A rocket gun follow -up signal and an accuse chronogenesis detector |
| CN105572481A (en) * | 2015-12-25 | 2016-05-11 | 哈尔滨工业大学 | Guided ammunition multipath sequential state signal measuring circuit and measuring method |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111312006A (en) * | 2020-03-03 | 2020-06-19 | 上海机电工程研究所 | Teaching demonstration device and method for mixed loading and launching control of multiple weapons |
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| Publication number | Publication date |
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| CN106091810A (en) | 2016-11-09 |
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