CN113028896A - Missile launching device outfield diagnosis system and method - Google Patents
Missile launching device outfield diagnosis system and method Download PDFInfo
- Publication number
- CN113028896A CN113028896A CN202110268433.5A CN202110268433A CN113028896A CN 113028896 A CN113028896 A CN 113028896A CN 202110268433 A CN202110268433 A CN 202110268433A CN 113028896 A CN113028896 A CN 113028896A
- Authority
- CN
- China
- Prior art keywords
- module
- diagnosis device
- missile
- zigbee
- processor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
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
- F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention provides a missile launcher outfield diagnosis system and method, comprising a fault diagnosis device and an onboard display; the fault diagnosis device comprises a diagnosis device processor, a first ZigBee receiving module and a first ZigBee transmitting module, wherein the diagnosis device processor is respectively connected with the first ZigBee receiving module and the first ZigBee transmitting module; the on-board display comprises an on-board display processor, a display module and a keyboard control module, wherein the display module and the keyboard control module are connected with the on-board display processor, and the on-board display processor is further connected with a second ZigBee receiving module and a second ZigBee transmitting module. The invention realizes the wireless connection between the small display and the missile launching system outfield diagnosis device by the Zigbee technology, reduces the dependence on the small display connection cable, improves the flexibility of field operators, and reduces the accident rate.
Description
Technical Field
The invention relates to the technical field of missile comprehensive test systems, in particular to a missile launching device outfield diagnosis system and method.
Background
The missile launching system is used as an important component of an airborne weapon system and is used as an interface between an airplane and a missile, the launching system directly determines whether the missile can normally work, and the health condition of the missile launching device needs to be diagnosed in order to ensure that the missile is launched smoothly and hits a target.
The missile launcher outfield diagnosis system is used for basic level (outfield) diagnosis, provides two functions of airplane diagnosis and airplane-launcher system diagnosis, the airplane diagnosis can diagnose functional components on the airplane which interact with the missile launcher system, the airplane-launcher system diagnosis can diagnose the launcher system which consists of the launcher and the functional components on the airplane which interact with the missile launcher system, the missile launcher outfield diagnosis system in service is provided with a small display, when the missile launcher system diagnoses faults in the outfield, the missile launcher outfield diagnosis system is connected with the missile launcher through a launcher diagnosis cable, the small display is connected with the diagnosis device through a small display connection cable, the diagnosis operation needs the cooperation of ground personnel and onboard operators to complete, the onboard operators operate the airplane in an airplane cockpit according to the display content of the small display, various required signals are provided for the missile launcher, and the small display can display the diagnosis result to an onboard operator.
The small display design using wired approach has the following disadvantages:
(1) the small display connecting cable stretches across between the aircraft cockpit and the missile launching system diagnosis device, so that the action flexibility of field personnel is reduced, and the accident probability of the field personnel is increased;
(2) the external field environment is severe, and in addition, due to the fact that an operator tramples on the cable accidentally, the cable is prone to failure, reliability is reduced, and normal use of the diagnosis device and normal training of troops are affected.
Disclosure of Invention
In view of the above, the invention provides a missile launching device external field diagnosis system and method, which realize wireless connection between a small display and a missile launching system external field diagnosis device through a Zigbee technology, reduce dependence on a small display connection cable, improve flexibility of field operators, and reduce accident rate.
In order to solve the technical problem, the invention provides a missile launching device outfield diagnosis system, which comprises a fault diagnosis device and an onboard display;
the fault diagnosis device comprises a diagnosis device processor, a first ZigBee receiving module and a first ZigBee transmitting module, wherein the diagnosis device processor is respectively connected with the first ZigBee receiving module and the first ZigBee transmitting module;
the on-board display comprises an on-board display processor, a display module and a keyboard control module, wherein the display module and the keyboard control module are connected with the on-board display processor, and the on-board display processor is further connected with a second ZigBee receiving module and a second ZigBee transmitting module.
Furthermore, the fault diagnosis device also comprises a missile simulation device, and the missile simulation device is connected with the diagnosis device processor.
Furthermore, the missile simulation device is electrically connected with the airborne missile launcher and is used for receiving the circuit working condition of the airborne missile launcher under actual operation and transmitting the circuit working condition back to the diagnostic device processor.
Further, the fault diagnosis device further comprises a power supply module, and the power supply module comprises a storage battery and a mains supply interface.
A missile launching device outfield diagnosis method comprises the following steps:
s1, wirelessly connecting the fault diagnosis device with the on-board display through the ZigBee receiving module and the ZigBee transmitting module;
s2, operating the fault diagnosis device by ground personnel, sending an instruction to the diagnosis device processor, sending the instruction to the on-board display processor through wireless transmission, and displaying the instruction by the on-board display processor through the control display module;
s3, operating the airborne missile launcher by an onboard operator through the keyboard control module according to the instruction, wherein the missile simulation device can receive the circuit working condition change of the airborne missile launcher;
and S4, the missile simulation device transmits the received circuit working condition change of the airborne missile launcher back to the fault diagnosis device for judgment, so that the missile launcher outfield diagnosis is realized.
The technical scheme of the invention has the following beneficial effects:
the fault diagnosis device is portable, gives the instruction through the fault diagnosis device, sends the instruction to the display on the aircraft through first zigBee transmitting module, and the personnel on the aircraft receive the instruction back through the display on the aircraft, according to the instruction operation, simultaneously on the opportunity the process that the display treater will operate sends the fault diagnosis device to supply ground personnel to look over through second zigBee transmitting module. The circuit working condition of the airborne missile launcher can be changed due to the operation condition of the personnel on the aircraft, and the fault diagnosis device is connected with the airborne missile launcher, so that the circuit working condition change of the airborne missile launcher can be checked, the received operation process can be checked, and the missile launching can be diagnosed.
The invention realizes the wireless connection between the small display and the missile launching system outfield diagnosis device by the Zigbee technology, reduces the dependence on the small display connection cable, improves the flexibility of field operators, and reduces the accident rate.
Drawings
FIG. 1 is a system block diagram of the missile launcher outfield diagnostic system of the present invention;
fig. 2 is a schematic structural diagram of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to fig. 1-2 of the embodiments of the present invention. It is to be understood that the embodiments described are only a few embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the described embodiments of the invention, are within the scope of the invention.
Example one
As shown in fig. 1-2: a missile launching device outfield diagnosis system comprises a fault diagnosis device and an onboard display;
the fault diagnosis device comprises a diagnosis device processor, a first ZigBee receiving module and a first ZigBee transmitting module, wherein the diagnosis device processor is respectively connected with the first ZigBee receiving module and the first ZigBee transmitting module;
the on-board display comprises an on-board display processor, a display module and a keyboard control module, wherein the display module and the keyboard control module are connected with the on-board display processor, and the on-board display processor is further connected with a second ZigBee receiving module and a second ZigBee transmitting module.
Specifically, the fault diagnosis device is portable, gives the instruction through the fault diagnosis device, sends the instruction to the display on the plane through first zigBee transmitting module, and the personnel on the plane receive the instruction back through the display on the plane, according to the instruction operation, simultaneously on the time the process that the display treater will operate sends the fault diagnosis device to supply ground personnel to look over through second zigBee transmitting module. The circuit working condition of the airborne missile launcher can be changed due to the operation condition of the personnel on the aircraft, and the fault diagnosis device is connected with the airborne missile launcher, so that the circuit working condition change of the airborne missile launcher can be checked, the received operation process can be checked, and the missile launching can be diagnosed.
According to one embodiment of the present invention, as shown in figures 1 and 2,
the fault diagnosis device further comprises a missile simulation device, and the missile simulation device is connected with the diagnosis device processor.
The missile simulation device is electrically connected with the airborne missile launcher and is used for receiving the circuit working condition of the airborne missile launcher under actual operation and transmitting the circuit working condition back to the diagnostic device processor.
The missile simulation device is electrically connected with the airborne missile launcher, so that the circuit working condition change of the airborne missile launcher can be monitored, and the change is transmitted back to the fault diagnosis device. The missile simulation device and the fault diagnosis device can be connected in a wireless or wired mode.
According to one embodiment of the present invention, as shown in figures 1 and 2,
the fault diagnosis device further comprises a power supply module, and the power supply module comprises a storage battery and a mains supply interface. The outfield is necessarily limited by conditions during diagnosis, so that the power supply of the fault diagnosis device adopts two modes, namely a mains supply interface and a storage battery, the mains supply interface is adopted for supplying power under the condition of mains supply, the storage battery supplies power under other conditions, the storage batteries can be prepared in advance, and the detection on multiple airplanes can be supported for a long time.
The embodiment provides a missile launching device external field diagnosis method, which comprises the following steps:
s1, wirelessly connecting the fault diagnosis device with the on-board display through the ZigBee receiving module and the ZigBee transmitting module;
s2, operating the fault diagnosis device by ground personnel, sending an instruction to the diagnosis device processor, sending the instruction to the on-board display processor through wireless transmission, and displaying the instruction by the on-board display processor through the control display module;
s3, operating the airborne missile launcher by an onboard operator through the keyboard control module according to the instruction, wherein the missile simulation device can receive the circuit working condition change of the airborne missile launcher;
and S4, the missile simulation device transmits the received circuit working condition change of the airborne missile launcher back to the fault diagnosis device for judgment, so that the missile launcher outfield diagnosis is realized.
In the present invention, unless otherwise explicitly specified or limited, for example, it may be fixedly attached, detachably attached, or integrated; can be mechanically or electrically connected; the terms may be directly connected or indirectly connected through an intermediate, and may be communication between two elements or interaction relationship between two elements, unless otherwise specifically limited, and the specific meaning of the terms in the present invention will be understood by those skilled in the art according to specific situations.
While the foregoing is directed to the preferred embodiment of the present invention, it will be understood by those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention as defined in the appended claims.
Claims (5)
1. A missile launcher outfield diagnostic system is characterized in that: the system comprises a fault diagnosis device and an on-board display;
the fault diagnosis device comprises a diagnosis device processor, a first ZigBee receiving module and a first ZigBee transmitting module, wherein the diagnosis device processor is respectively connected with the first ZigBee receiving module and the first ZigBee transmitting module;
the on-board display comprises an on-board display processor, a display module and a keyboard control module, wherein the display module and the keyboard control module are connected with the on-board display processor, and the on-board display processor is further connected with a second ZigBee receiving module and a second ZigBee transmitting module.
2. The missile launcher outfield diagnostic system of claim 1, wherein: the fault diagnosis device further comprises a missile simulation device, and the missile simulation device is connected with the diagnosis device processor.
3. The missile launcher outfield diagnostic system of claim 2, wherein: the missile simulation device is electrically connected with the airborne missile launcher and is used for receiving the circuit working condition of the airborne missile launcher under actual operation and transmitting the circuit working condition back to the diagnostic device processor.
4. The missile launcher outfield diagnostic system of claim 3, wherein: the fault diagnosis device further comprises a power supply module, and the power supply module comprises a storage battery and a mains supply interface.
5. A missile launcher outfield diagnostic method as defined in any one of claims 1 to 4 wherein: the method comprises the following steps:
s1, wirelessly connecting the fault diagnosis device with the on-board display through the ZigBee receiving module and the ZigBee transmitting module;
s2, operating the fault diagnosis device by ground personnel, sending an instruction to the diagnosis device processor, sending the instruction to the on-board display processor through wireless transmission, and displaying the instruction by the on-board display processor through the control display module;
s3, operating the airborne missile launcher by an onboard operator through the keyboard control module according to the instruction, wherein the missile simulation device can receive the circuit working condition change of the airborne missile launcher;
and S4, the missile simulation device transmits the received circuit working condition change of the airborne missile launcher back to the fault diagnosis device for judgment, so that the missile launcher outfield diagnosis is realized.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2020114006954 | 2020-12-04 | ||
| CN202011400695.4A CN112344793A (en) | 2020-12-04 | 2020-12-04 | Missile launching device outfield diagnosis system and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113028896A true CN113028896A (en) | 2021-06-25 |
| CN113028896B CN113028896B (en) | 2023-07-21 |
Family
ID=74428066
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011400695.4A Pending CN112344793A (en) | 2020-12-04 | 2020-12-04 | Missile launching device outfield diagnosis system and method |
| CN202110268433.5A Active CN113028896B (en) | 2020-12-04 | 2021-03-11 | Guided missile launching device outfield diagnosis system and method |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011400695.4A Pending CN112344793A (en) | 2020-12-04 | 2020-12-04 | Missile launching device outfield diagnosis system and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN112344793A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5414347A (en) * | 1992-07-13 | 1995-05-09 | Hughes Aircraft Company | Method and apparatus for missile interface testing |
| US20050081733A1 (en) * | 2003-08-13 | 2005-04-21 | Leonard James V. | Methods and apparatus for testing and diagnosis of weapon control systems |
| US20100209880A1 (en) * | 2009-02-19 | 2010-08-19 | James Victor Leonard | Missile simulator |
| CN111630951B (en) * | 2013-07-10 | 2015-05-20 | 中国航天科工集团第三研究院第八三五七研究所 | Airborne physical-free fire control simulation training method |
| CN106643294A (en) * | 2017-02-09 | 2017-05-10 | 沈阳航空航天大学 | Dual-mode launcher for airborne missile |
| CN109035737A (en) * | 2018-08-31 | 2018-12-18 | 西安航天动力技术研究所 | A kind of wireless transmission control system based on ZigBee technology |
| CN111190416A (en) * | 2020-02-20 | 2020-05-22 | 南昌航空大学 | Ground detection device and detection method for airborne fire control system |
| CN111516904A (en) * | 2020-05-22 | 2020-08-11 | 山东首景辉光电科技有限公司 | Device for detecting interference bomb releasing equipment of military aircraft based on ZigBee |
| CN214620859U (en) * | 2020-12-04 | 2021-11-05 | 中国人民解放军空军工程大学航空机务士官学校 | Missile launcher outfield diagnostic system |
-
2020
- 2020-12-04 CN CN202011400695.4A patent/CN112344793A/en active Pending
-
2021
- 2021-03-11 CN CN202110268433.5A patent/CN113028896B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5414347A (en) * | 1992-07-13 | 1995-05-09 | Hughes Aircraft Company | Method and apparatus for missile interface testing |
| US20050081733A1 (en) * | 2003-08-13 | 2005-04-21 | Leonard James V. | Methods and apparatus for testing and diagnosis of weapon control systems |
| US20100209880A1 (en) * | 2009-02-19 | 2010-08-19 | James Victor Leonard | Missile simulator |
| CN111630951B (en) * | 2013-07-10 | 2015-05-20 | 中国航天科工集团第三研究院第八三五七研究所 | Airborne physical-free fire control simulation training method |
| CN106643294A (en) * | 2017-02-09 | 2017-05-10 | 沈阳航空航天大学 | Dual-mode launcher for airborne missile |
| CN109035737A (en) * | 2018-08-31 | 2018-12-18 | 西安航天动力技术研究所 | A kind of wireless transmission control system based on ZigBee technology |
| CN111190416A (en) * | 2020-02-20 | 2020-05-22 | 南昌航空大学 | Ground detection device and detection method for airborne fire control system |
| CN111516904A (en) * | 2020-05-22 | 2020-08-11 | 山东首景辉光电科技有限公司 | Device for detecting interference bomb releasing equipment of military aircraft based on ZigBee |
| CN214620859U (en) * | 2020-12-04 | 2021-11-05 | 中国人民解放军空军工程大学航空机务士官学校 | Missile launcher outfield diagnostic system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113028896B (en) | 2023-07-21 |
| CN112344793A (en) | 2021-02-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN214620859U (en) | Missile launcher outfield diagnostic system | |
| CN106323104B (en) | Missile ground comprehensive testing device and method based on wireless network | |
| CN102799175B (en) | Rapid detection device and detection method for unmanned aircraft system | |
| CN107544458B (en) | Airborne detection device and detection method for air-to-air missile | |
| CN111190416A (en) | Ground detection device and detection method for airborne fire control system | |
| CN204189339U (en) | A kind of airborne electronic equipment Jamming pod safeguards training system | |
| CN106292589B (en) | A kind of redundancy management method of the manual intervention applied to unmanned plane | |
| CN113028896A (en) | Missile launching device outfield diagnosis system and method | |
| KR102392250B1 (en) | Fire fighting special vehicle for remote self-diagnosis and monitoring system thereof | |
| CN211001884U (en) | Unmanned aerial vehicle retrieves device | |
| CN211207168U (en) | Airborne fire control system ground detection device | |
| US9521374B1 (en) | Real time relative performance indication for redundant avionics optical data transmission systems for aerial refueling remote vision systems | |
| CN106814728A (en) | A kind of assembly detection apparatus based on product power supply interface sequential logic | |
| CN110887670B (en) | Aircraft engine propeller test system | |
| CN210555627U (en) | Unmanned aerial vehicle transmission controlling means | |
| CN100565402C (en) | The method and apparatus that is used for testing valve control system | |
| CN207965631U (en) | A kind of wireless telecommunications automotive diagnostic system | |
| CN105736792A (en) | Control device for multi-channel electromagnetic valve | |
| CN110789725A (en) | Communication equipment for civil aviation passenger plane | |
| CN220273795U (en) | Telemetry data monitoring system | |
| CN104867259A (en) | Unmanned aircraft remote controller light warning system | |
| CN206517446U (en) | A kind of unmanned plane cloud monitoring system | |
| CN112034747A (en) | WiFi-based portable unmanned aerial vehicle test system | |
| CN214067618U (en) | Multi-repeating-emission measurement and launch control system | |
| CN218499144U (en) | Redundant backup device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |