CN113028896B - Guided missile launching device outfield diagnosis system and method - Google Patents
Guided missile launching device outfield diagnosis system and method Download PDFInfo
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- CN113028896B CN113028896B CN202110268433.5A CN202110268433A CN113028896B CN 113028896 B CN113028896 B CN 113028896B CN 202110268433 A CN202110268433 A CN 202110268433A CN 113028896 B CN113028896 B CN 113028896B
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- 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
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- 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 launching device 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 also connected with a second ZigBee receiving module and a second ZigBee transmitting module. According to the invention, the wireless connection between the small display and the external field diagnosis device of the missile launching system is realized through the Zigbee technology, so that the dependence on a small display connection cable is reduced, the flexibility of field operators is improved, and the accident rate is reduced.
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 quality of the launching system directly determines whether the missile can normally work, and in order to ensure that the missile is launched smoothly and hits a target, the health condition of the missile launching device needs to be diagnosed.
The missile launching device external field diagnosis system is used for basic level (external field) diagnosis, provides two functions of airplane diagnosis and airplane-launching device system diagnosis, the airplane diagnosis can be realized on functional components on an airplane which interact with the missile launching system, the airplane-launching device system diagnosis can be realized on the launching system which consists of a launching device and the functional components on the airplane which interact with the missile launching system, the active missile launching device external field diagnosis system is provided with a small display, when the missile launching system performs fault diagnosis in an external field, the missile launching device external field diagnosis system is connected with the missile launching device through a launching frame diagnosis cable, the small display is connected with the diagnosis device through a small display connection cable, the diagnosis operation is completed by cooperation of ground personnel and on-board operators, the on-board operators operate the airplane in an airplane cockpit according to the display content of the small display, the missile launching frame is provided with various required signals, and the small display can display diagnosis results to the on-board operators.
The small display design using the wired approach has the following drawbacks:
(1) The small display connecting cable spans between the aircraft cockpit and the missile launching system diagnosis device, so that the mobility and flexibility of on-site personnel are reduced, and meanwhile, the probability of accidents of the on-site personnel is increased;
(2) The external field environment is bad, and the cable is easy to break down due to the fact that operators step on the cable unintentionally, 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 outfield diagnosis system and method, which realize wireless connection of a small display and the missile launching system outfield diagnosis device through Zigbee technology, reduce dependence on a small display connection cable, improve flexibility of field operators and reduce accident occurrence rate.
In order to solve the technical problems, 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 also connected with a second ZigBee receiving module and a second ZigBee transmitting module.
Furthermore, the fault diagnosis device further comprises a missile simulation device, and the missile simulation device is connected with the diagnosis device processor.
Further, 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 processor of the diagnosis device.
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 a fault diagnosis device with an on-board display through a ZigBee receiving module and a ZigBee transmitting module;
s2, operating the fault diagnosis device by ground personnel, issuing an instruction to a diagnosis device processor, transmitting the instruction to an on-board display processor through wireless transmission, and displaying by the on-board display processor through a control display module;
s3, an onboard operator operates the airborne missile launcher according to the instruction through the keyboard control module, and the missile simulation device can receive the change of the circuit working condition of the airborne missile launcher;
s4, the missile simulation device transmits the received circuit working condition change of the airborne missile launching frame back to the fault diagnosis device for judgment, so that the outfield diagnosis of the missile launching device is realized.
The technical scheme of the invention has the following beneficial effects:
the fault diagnosis device is portable, an instruction is issued through the fault diagnosis device, the instruction is sent to the on-board display through the first ZigBee transmitting module, after receiving the instruction through the on-board display, an on-board person operates according to the instruction, and the on-board display processor sends an operation process to the fault diagnosis device through the second ZigBee transmitting module at the same time for the ground person to check. The condition of the operation of the personnel on the aircraft can cause the change of the circuit working condition of the missile launcher on the aircraft, and the fault diagnosis device is connected with the missile launcher on the aircraft so as to check the change of the circuit working condition and check the received operation process, thereby diagnosing the missile launching.
According to the invention, the wireless connection between the small display and the external field diagnosis device of the missile launching system is realized through the Zigbee technology, so that the dependence on a small display connection cable is reduced, the flexibility of field operators is improved, and the accident rate is reduced.
Drawings
FIG. 1 is a system block diagram of a missile launcher outfield diagnostic system of the present invention;
fig. 2 is a schematic structural view of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention more clear, 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 will be apparent that the described embodiments are some, but not all, embodiments of the invention. All other embodiments, which are obtained by a person skilled in the art based on the described embodiments of the invention, fall within the scope of protection of the invention.
Example 1
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 also connected with a second ZigBee receiving module and a second ZigBee transmitting module.
Specifically, the fault diagnosis device is portable, an instruction is issued through the fault diagnosis device, the instruction is sent to the on-board display through the first ZigBee transmitting module, after receiving the instruction through the on-board display, an on-board person operates according to the instruction, and the on-board display processor sends an operation process to the fault diagnosis device through the second ZigBee transmitting module at the same time for the ground person to check. The condition of the operation of the personnel on the aircraft can cause the change of the circuit working condition of the missile launcher on the aircraft, and the fault diagnosis device is connected with the missile launcher on the aircraft so as to check the change of the circuit working condition and check the received operation process, thereby diagnosing the missile launching.
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 processor of the diagnosis device.
The missile simulation device is electrically connected with the airborne missile launcher, so that the change of the working condition of a circuit 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 external field diagnosis is necessarily limited by conditions, 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, and the storage battery is used for supplying power under other conditions, so that a plurality of storage batteries can be prepared in advance, and the fault diagnosis device can support long-time detection and detection of multiple aircrafts.
The embodiment provides a missile launching device outfield diagnosis method, which comprises the following steps:
s1, wirelessly connecting a fault diagnosis device with an on-board display through a ZigBee receiving module and a ZigBee transmitting module;
s2, operating the fault diagnosis device by ground personnel, issuing an instruction to a diagnosis device processor, transmitting the instruction to an on-board display processor through wireless transmission, and displaying by the on-board display processor through a control display module;
s3, an onboard operator operates the airborne missile launcher according to the instruction through the keyboard control module, and the missile simulation device can receive the change of the circuit working condition of the airborne missile launcher;
s4, the missile simulation device transmits the received circuit working condition change of the airborne missile launching frame back to the fault diagnosis device for judgment, so that the outfield diagnosis of the missile launching device is realized.
In the present invention, unless explicitly specified and defined otherwise, for example, it may be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intermediaries, or in communication with each other or in interaction with each other, unless explicitly defined otherwise, the meaning of the terms described above in this application will be understood by those of ordinary skill in the art in view of the specific circumstances.
While the foregoing is directed to the preferred embodiments of the present invention, it will be appreciated by those skilled in the art that various modifications and adaptations can be made without departing from the principles of the present invention, and such modifications and adaptations are intended to be comprehended within the scope of the present invention.
Claims (2)
1. A missile launcher outfield diagnostic system, characterized by: 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 also connected with a second ZigBee receiving module and a second ZigBee transmitting module;
the fault diagnosis device further comprises a missile simulation device, and the missile simulation device is connected with a 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 processor of the diagnosis device;
the missile launcher outfield diagnostic system comprises the following steps when in use:
s1, wirelessly connecting a fault diagnosis device with an on-board display through a ZigBee receiving module and a ZigBee transmitting module;
s2, operating the fault diagnosis device by ground personnel, issuing an instruction to a diagnosis device processor, transmitting the instruction to an on-board display processor through wireless transmission, and displaying by the on-board display processor through a control display module;
s3, an onboard operator operates the airborne missile launcher according to the instruction through the keyboard control module, and the missile simulation device can receive the change of the circuit working condition of the airborne missile launcher;
s4, the missile simulation device transmits the received circuit working condition change of the airborne missile launching frame back to the fault diagnosis device for judgment, so that the outfield diagnosis of the missile launching device is realized.
2. The missile launcher outfield diagnostic system of claim 1, 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.
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 |
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| Publication Number | Publication Date |
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| CN113028896A CN113028896A (en) | 2021-06-25 |
| CN113028896B true CN113028896B (en) | 2023-07-21 |
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| 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 |
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| CN202011400695.4A Pending CN112344793A (en) | 2020-12-04 | 2020-12-04 | Missile launching device outfield diagnosis system and method |
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Citations (3)
| 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 |
| 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 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7228261B2 (en) * | 2003-08-13 | 2007-06-05 | The Boeing Company | Methods and apparatus for testing and diagnosis of weapon control systems |
| US8714979B2 (en) * | 2009-02-19 | 2014-05-06 | The Boeing Company | 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 |
| CN106643294B (en) * | 2017-02-09 | 2018-01-16 | 沈阳航空航天大学 | A kind of airborne missile double mode emitter |
| 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
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2021
- 2021-03-11 CN CN202110268433.5A patent/CN113028896B/en active Active
Patent Citations (3)
| 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 |
| 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 |
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| Publication number | Publication date |
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| CN113028896A (en) | 2021-06-25 |
| CN112344793A (en) | 2021-02-09 |
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