CN106091810A - 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
- CN106091810A CN106091810A CN201610391624.XA CN201610391624A CN106091810A CN 106091810 A CN106091810 A CN 106091810A CN 201610391624 A CN201610391624 A CN 201610391624A CN 106091810 A CN106091810 A CN 106091810A
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- Prior art keywords
- way
- module
- missile launching
- series rules
- missile
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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
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
- Toys (AREA)
Abstract
The open a kind of four-way MISSILE LAUNCHING time-series rules module of the present invention, the MISSILE LAUNCHING sequential of four passages can be detected simultaneously, externally forwarded testing result by CAN, simultaneously according to the MISSILE LAUNCHING sequential of respective channel, provide guided missile springing signal in real time.This four-way MISSILE LAUNCHING time-series rules module employing TMS320F28335 DSP is as master controller, including four transmitted in both directions devices, DC/DC device, ferroelectric memory, CAN driving element, electromagnetic relay unit device and functional circuit.Rectangular connector of the present invention and modular structure, higher compared to prior art, vibration resistance and thermal diffusivity, maintainability, protection are more preferable.
Description
Technical field
The present invention relates to ground launch and control technical field, particularly to a kind of four-way MISSILE LAUNCHING time-series rules mould
Block.
Background technology
Launching sequential is to pass judgment on the critical data of guided missile whether normal transmission.Launching time sequence detecting circuit is launching control system weight
Want ingredient, from the beginning of launching control system performs " launch and make ", terminate after " missile takeoff ", supply launching flow process Zhong Ge road
The igniting of electricity, priming system and firing box (cylinder) and guided missile are electrically returned the state of announcement and are detected, and then testing result formation are sent out
Penetrate sequential to preserve.
The transmitting time-series rules functional circuit of current launching control system is general is coupling in one with transmitting flow performing functional circuit
Rise, use identical benchmark job power supply, controlled by same controller, collectively constituted the repertoire of launching control system.Send out
Penetrate time sequence detecting circuit and abnormal (such as testing circuit short circuit or being disturbed by external signal) once occurs, frequently can lead to other merit
Energy circuit operation irregularity, even there will be director demon and runs " deadlock " phenomenon.Additionally, flow performing mistake launched by controller
Once occurring exception in journey, causing launching time series data cannot collect, and technical problem analysis will be extremely difficult afterwards.
Summary of the invention
The present invention is to solve current launch other functional circuit of time sequence detecting circuit and launching control system couple cause
Ore-controlling Role work basic reliability reduces problem, it is provided that a kind of four-way MISSILE LAUNCHING time-series rules module, will launch sequential inspection
Slowdown monitoring circuit is independent, on the premise of not affecting launching control system work basic reliability, completes MISSILE LAUNCHING time-series rules merit
Energy.
In order to arrive above-mentioned purpose, the technical scheme is that a kind of four-way MISSILE LAUNCHING time-series rules mould of offer
Block, wherein comprises and is arranged in a housing: master controller and the ferroelectric memory being connected respectively with this master controller, DC/
DC change-over circuit, springing output control circuit, CAN drive change-over circuit and four transmitted in both directions devices；Each transmitted in both directions device
16 tunnels of a corresponding execution passage are launched clock signal and are acquired by part；Detection module passes through described housing plug-in mounting
In the pedestal matched with this housing.
Preferably, the front side of described hull outside is provided with the socket piece of rectangular electric connector as output interface, described inserts
Seat piece is with guide finger；The patch bay of described pedestal is provided with defeated as follow-up components and parts of the plug piece of rectangular electric connector
Incoming interface, described plug piece is with fairlead；In pedestal during plug-in mounting detection module, with guide finger socket piece with leading
Plug piece to set matches, and provides for grafting electric connector and guides.
Preferably, upper rail groove that the both sides up and down of described hull outside are correspondingly arranged and lower guideway groove, with described pedestal
Internal up and down upper rail and the lower guideway that both sides are arranged is respectively cooperating with, and provides for plug-in mounting detection module in pedestal and guides.
Preferably, the rear side of described housing is provided with rivet coating nut and equipped with corresponding captive screw, it is possible in detection
Module plugs together and after putting in place fastens this detection module.
Preferably, the rear side of described housing is provided with handle, provides impetus for module plug.
Preferably, at the bottom of the inside at described housing is provided with the CPU board containing master controller and the detection containing transmitted in both directions device
Plate；By pyrite hexagonal spacer, detection base plate is anchored on the inner surface of described housing, and makes CPU board stack to be arranged in this
On detection base plate, and guarantee distance spaced between CPU board and detection base plate；Described DC/DC change-over circuit is set
Module, is additionally connected to other positions that case inside surface is not connected with detection base plate.
Preferably, described master controller uses the dsp chip of TMS320F28335.
Preferably, described transmitted in both directions device uses 74ALVC164245 acquisition chip.
Preferably, described 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, have the advantage that
1 is completely isolated with other functional circuit of launching control system, neither affects other functional circuit and normally works, the most not by it
Its functional circuit impact, enhances the basic reliability of launching control system.
2, possess and complete four passages simultaneously, the transmitting clock signal acquisition function on each passage 16 tunnel, it is possible to by sequential
Testing result preserves, and can be by CAN in real time by time-series rules result outgoing, it is possible to adapt to current main-stream ground (warship)
Time-series rules demand launched by face armament systems.
3, process guide-track groove on module housing, install and process guide rail on the pedestal of module, lead for module plug offer
To, it is achieved blind plugging function, easy to operate.
4, the socket piece of the rectangular electric connector of one band guide finger of employing guides as the output interface of module, a band
The plug piece of the rectangular electric connector of set and spring assembly, as the input interface of follow-up components and parts, can evade adapter folder dead
Risk, height vibration, impact complex environment in, it is ensured that the signal seriality of adapter and high reliability.
Accompanying drawing explanation
Fig. 1 is the circuit theory diagrams of the present invention a kind of four-way MISSILE LAUNCHING time-series rules module.
Fig. 2, Fig. 3 are the threedimensional models in the present invention a kind of four-way MISSILE LAUNCHING time-series rules mould former and later two directions outside
Figure.
Fig. 4 is the three-dimensional model diagram within the present invention a kind of four-way MISSILE LAUNCHING time-series rules mould.
Fig. 5 is the scheme of installation of the present invention a kind of four-way MISSILE LAUNCHING time-series rules module.
Detailed description of the invention
By describing the technology contents of the present invention, structural feature in detail, being reached purpose and effect, give below in conjunction with accompanying drawing
To describe in detail.
Refer to shown in Fig. 1, four-way MISSILE LAUNCHING time-series rules module (the following or referred to as detection that the present invention proposes
Module), use TMS320F28335 DSP(Digital Signal Processing) chip is as master controller 11, and it is provided with four be attached thereto
Individual transmitted in both directions device 12, ferroelectric memory 13, DC/DC change-over circuit 14, springing output control circuit 15, CAN drive conversion
Circuit 16.
Possessing four and perform passage, clock signal is launched, by corresponding with this execution passage in 16 tunnels of each execution passage
A transmitted in both directions device 12 be acquired.The logic level of DSP is 3.3V, and outside acquisition chip is 5V running voltage.This
Transmitted in both directions device 12 in example uses 74ALVC164245 chip, had both solved the voltage matches problem of signals collecting, and had also subtracted
Lack circuit scale and number of chips, low in energy consumption, highly versatile.Use ferroelectric memory 13, it is achieved enter launching timing results
The function of row memory storage.
Refer to shown in Fig. 2, Fig. 3, it is shown that the external structure of the housing 20 of detection module of the present invention, this housing 20
Both sides are correspondingly arranged on upper rail groove 21 and lower guideway groove 22 up and down, it is possible to the upper rail set by pedestal and lower guideway difference
Coordinate, provide for plug-in mounting detection module on pedestal and guide.The rear side of housing 20 is provided with several rivet coating nuts 23 each autogamy
Standby captive screw, it is possible to after detection module plugs together and puts in place, this module is fastened；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, above with guide finger
26, provide for grafting electric connector and guide.
Refer to shown in Fig. 4, inside the housing 20 of detection module, by several pyrite hexagonal spacers 34, will arrange
The detection base plate of transmitted in both directions device (and ferroelectric memory, springing output control circuit, CAN drive the parts such as change-over circuit)
32 are anchored on the inner surface of housing 20 of detection module, and are that the CPU board 31 being provided with master controller provides installation position
Put, make CPU board 31 stack and be arranged on detection base plate 32 and and detect distance spaced between base plate 32；DC/ is set
The module 33 of DC change-over circuit is additionally connected to other positions of housing 20 inner surface.
Refer to shown in Fig. 5, for the pedestal 40 of plug-in mounting detection module, be provided with patch bay 41；Pedestal about 40
The inner surface of both sides is correspondingly arranged on upper rail and lower guideway 42, it is possible to upper rail groove and the lower guideway of detection module housing 20
Groove matches, and provides for plug-in mounting module and guides.Patch bay 41 is provided with multiple installation site, at least one of which installation position
Installing the plug piece 43 of rectangular electric connector, the plug piece 43 of this rectangular electric connector is with fairlead 44；Other installation positions
Put and can be used to arrange other detection modules or arrange other functional modules of launching control system.
In detection module is inserted to pedestal 40, the socket piece 25 of rectangular electric connector on detection module housing 20, it is possible to
Match with the plug piece 43 of rectangular electric connector installed on patch bay 41, and the guide finger 26 of socket piece 25 and plug
The fairlead 44 of part 43 matches, and provides for grafting electric connector and guides, thus realizes blind plugging function.Fairlead 44 is provided with bullet
Spring assembly.
Wherein, the socket piece 25 of the rectangular electric connector of band guide finger 26 is as the output interface of module, band fairlead 44
With the plug piece 43 of the rectangular electric connector of spring assembly as the input interface of follow-up components and parts, enhance the vibration resistance of equipment
And thermal diffusivity, improve the maintainability of equipment, protection level.
In sum, the present invention carries out modularized design to MISSILE LAUNCHING time sequence detecting circuit, uses independent work base
Quasi-power supply, independent controller, be suitable to (warship) face missile armament emission system, it is possible to complete sending out of guided missile to four passages
Penetrate time-series rules function.Detection module housing uses boxlike dongle configuration, utilizes guide finger to position, it is possible to achieve blindmate and anti-error
Insert.
Although present disclosure has been made to be 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 foregoing, for the present invention's
Multiple amendment and replacement all will be apparent from.Therefore, protection scope of the present invention should be limited to the appended claims.
Claims (9)
1. a four-way MISSILE LAUNCHING time-series rules module, it is characterised in that comprise and be arranged in a housing: main control
Device and the ferroelectric memory being connected respectively with this master controller, DC/DC change-over circuit, springing output control circuit, CAN drive and turn
Change circuit and four transmitted in both directions devices；When 16 tunnels of a corresponding execution passage are launched by each transmitted in both directions device
Sequential signal is acquired；Detection module is inserted in the pedestal matched with this housing by described housing.
2. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The front side of described hull outside is provided with the socket piece of rectangular electric connector as output interface, and described socket piece is with guiding
Pin；The patch bay of described pedestal is provided with the plug piece input interface as follow-up components and parts of rectangular electric connector, described
Plug piece is with fairlead；In pedestal during plug-in mounting detection module, the socket piece with guide finger and the plug with fairlead
Part matches, and provides for grafting electric connector and guides.
3. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1 or 2, it is characterised in that
Upper rail groove that the both sides up and down of described hull outside are correspondingly arranged and lower guideway groove, both sides upper and lower with described base interior
The upper rail and the lower guideway that arrange are respectively cooperating with, and provide for plug-in mounting detection module in pedestal and guide.
4. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The rear side of described housing is provided with rivet coating nut and equipped with corresponding captive screw, it is possible to plugs together at detection module and puts in place
Afterwards this detection module is fastened.
5. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The rear side of described housing is provided with handle, provides impetus for module plug.
6. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
The CPU board containing master controller and the detection base plate containing transmitted in both directions device it is provided with in the inside of described housing；Pass through pyrite
Hexagonal spacer, is anchored on the inner surface of described housing by detection base plate, and make CPU board stack be arranged in this detection base plate it
On, and guarantee distance spaced between CPU board and detection base plate；The module of described DC/DC change-over circuit is set, additionally connects
It is connected on other positions that case inside surface is not connected with detection base plate.
7. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
Described master controller uses the dsp chip of TMS320F28335.
8. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
Described transmitted in both directions device uses 74ALVC164245 acquisition chip.
9. four-way MISSILE LAUNCHING time-series rules module as claimed in claim 1, it is characterised in that
Described 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 true CN106091810A (en) | 2016-11-09 |
| CN106091810B 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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| Country | Link |
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| CN (1) | CN106091810B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114268582A (en) * | 2021-11-24 | 2022-04-01 | 上海机电工程研究所 | Springing forwarding system and device |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111312006B (en) * | 2020-03-03 | 2022-03-18 | 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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| 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 (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114268582A (en) * | 2021-11-24 | 2022-04-01 | 上海机电工程研究所 | Springing forwarding system and device |
| 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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| Publication number | Publication date |
|---|---|
| CN106091810B (en) | 2017-10-10 |
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