CN110697074A - Aircraft testing device capable of realizing human-computer real-time interaction - Google Patents
Aircraft testing device capable of realizing human-computer real-time interaction Download PDFInfo
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- CN110697074A CN110697074A CN201910931306.1A CN201910931306A CN110697074A CN 110697074 A CN110697074 A CN 110697074A CN 201910931306 A CN201910931306 A CN 201910931306A CN 110697074 A CN110697074 A CN 110697074A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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Abstract
The invention discloses an aircraft testing device capable of realizing human-computer real-time interaction, which comprises a control host, a cloud server, a testing device main body and a data acquisition device, wherein the control host is respectively connected with the cloud server and the testing device main body through a network; the testing device main body comprises a flight parameter acquisition module, an aircraft motion capture module and a data management module. The invention comprises a testing device main body and a data acquisition device, wherein the data acquisition device can be directly plugged on an aircraft for use due to small volume, and feeds acquired data back to the testing device main body in real time, thereby realizing real-time data feedback and being beneficial to analysis of a testing result.
Description
Technical Field
The invention relates to the technical field of aircraft testing, in particular to an aircraft testing device capable of realizing human-computer real-time interaction.
Background
Aircraft testing refers to the full testing of aircraft according to specified technical requirements and specific specified stacks. The main items of the test comprise a system test, a flight test and a comprehensive test. Only the tested aircraft can ensure the purposes of flight safety and risk control.
At present, the test of the aircraft is mainly performed through a test platform, the test platform is connected with the aircraft through a data line, when the aircraft is started, data of the aircraft are directly acquired, and because the test environment of the aircraft is greatly different from the real environment, equipment for testing the aircraft in the real environment and performing data interaction with the test platform in real time is needed.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides an aircraft testing device capable of realizing man-machine real-time interaction.
The purpose of the invention is realized by the following technical scheme:
an aircraft testing device capable of realizing human-computer real-time interaction comprises a control host, a cloud server, a testing device body and a data acquisition device, wherein the control host is respectively connected with the cloud server and the testing device body through a network; the testing device main body comprises a flight parameter acquisition module, an aircraft motion capture module and a data management module; the flight parameter acquisition module comprises an inclination angle detection sensor, a photosensitive detection device and a laser capture device, and the aircraft motion capture module comprises an optical image capture analysis module and an infrared capture module; the data management module comprises a processor, a first storage device and a second storage device, wherein the first storage device and the second storage device are respectively connected with the processor; the processor is provided with a data test socket;
the data acquisition device comprises a miniature shell and a PCB (printed Circuit Board) arranged in the miniature shell, wherein one end of the miniature shell is provided with a plug-in port used for being fixedly connected to an aircraft, and the miniature shell is also provided with an anti-falling device.
Furthermore, the anti-disengaging device is a magnetic attraction piece, the magnetic attraction piece is arranged on the upper surface of the miniature shell, and the magnetic attraction piece is correspondingly connected with the magnetic attraction patch on the aircraft.
Further, the interface includes a USB interface.
Furthermore, the edge of the plug interface is provided with an anti-falling lock catch which is embedded in the plug groove of the aircraft and is buckled with the edge of the plug groove to realize locking.
Furthermore, the data acquisition device comprises a gyroscope, an acceleration sensor and a data memory, the gyroscope and the acceleration sensor are respectively connected with the processor, and the processor is also in data interconnection with the data memory.
Further, the data acquisition device comprises a wireless transmission module, and the wireless transmission module comprises a 5G/4G/3G module, a Bluetooth module or a WIFI communication module.
Furthermore, a control handle is arranged on the control host, and the control handle sends a control command to the testing device main body through a network.
The invention has the beneficial effects that:
(1) the device comprises a testing device body and a data acquisition device, wherein the data acquisition device can be directly inserted into an aircraft for use due to small volume, and feeds acquired data back to the testing device body in real time, so that real-time data feedback is realized, and analysis of a testing result is facilitated;
(2) the testing device main body comprises a flight parameter acquisition module, an aircraft motion capture module and a data management module, and can detect the inclination angle of the aircraft, analyze the photosensitive performance, capture the motion and the like.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a block diagram of a testing device body according to the present invention;
FIG. 3 is a block diagram of a flight parameter module of the present invention;
in the figure, 10-control host, 11-cloud server, 12-test device body, 13-data acquisition device, 14-flight parameter module, 15-aircraft motion capture module, 16-data management module, 17-inclination detection sensor, 18-photosensitivity detection device and 19-laser capture device.
Detailed Description
The technical solutions of the present invention are further described in detail below with reference to the accompanying drawings, but the scope of the present invention is not limited to the following.
Example 1:
the embodiment provides an aircraft testing device capable of realizing human-computer real-time interaction, which is shown in fig. 1-fig. 3 and comprises a control host 10, a cloud server 11, a testing device main body 12 and a data acquisition device 13, wherein the control host 10 is respectively connected with the cloud server 11 and the testing device main body 12 through a network, the testing device main body 12 is in data interconnection with the data acquisition device 13 through the network, and the data acquisition device 13 is installed on an aircraft and moves along with the movement of the aircraft; the testing device main body 12 comprises a flight parameter acquisition module 14, an aircraft motion capture module 15 and a data management module 16; the flight parameter acquisition module 14 comprises an inclination angle detection sensor 17, a photosensitive detection device 18 and a laser capture device 19, and the aircraft motion capture module 15 comprises an optical image capture analysis module and an infrared capture module; the data management module 16 comprises a processor, a first storage device and a second storage device, wherein the first storage device and the second storage device are respectively connected with the processor; the processor is provided with a data test socket;
the data acquisition device comprises a miniature shell and a PCB (printed Circuit Board) arranged in the miniature shell, wherein one end of the miniature shell is provided with a plug-in port used for being fixedly connected to an aircraft, and the miniature shell is also provided with an anti-falling device.
This embodiment includes testing arrangement main part 12 and data acquisition device 13, and data acquisition device 13 can directly peg graft and use on the aircraft because small in size, and data acquisition device 13 feeds back the data of gathering to testing arrangement main part 12 in real time, realizes real-time data feedback, is favorable to the analysis of test result.
Example 2:
this embodiment still includes that the anticreep device inhales the piece for the magnetism on embodiment 1's basis, and the piece is inhaled to magnetism locates miniature casing's upper surface, and the magnetism inhales the piece and inhales the paster position correspondence with the magnetism on the aircraft and link to each other, and the interface includes the USB interface, and the interface edge is equipped with the anticreep hasp, and the anticreep hasp inlays in the grafting recess of aircraft to realize the locking with the marginal looks lock of grafting recess.
Further, the data acquisition device 13 includes a gyroscope, an acceleration sensor and a data storage, the gyroscope and the acceleration sensor are respectively connected with the processor, and the processor is also interconnected with the data storage.
Further, the data acquisition device 13 comprises a wireless transmission module, and the wireless transmission module comprises a 5G/4G/3G module, a Bluetooth module or a WIFI communication module.
Further, the control host 10 is provided with a control handle, and the control handle sends a control command to the test device main body through a network.
The device comprises a testing device main body 12 and a data acquisition device 13, wherein the data acquisition device 13 can be directly inserted into an aircraft for use due to small volume, and the data acquisition device 13 feeds acquired data back to the testing device main body 12 in real time, so that real-time data feedback is realized, and analysis of a testing result is facilitated; the testing device main body comprises a flight parameter acquisition module, an aircraft motion capture module and a data management module, and can detect the inclination angle of the aircraft, analyze the photosensitive performance, capture the motion and the like.
The above-mentioned embodiments only express the specific embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the present invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention.
Claims (7)
1. An aircraft testing device capable of realizing human-computer real-time interaction is characterized by comprising a control host, a cloud server, a testing device body and a data acquisition device, wherein the control host is respectively connected with the cloud server and the testing device body through a network; the testing device main body comprises a flight parameter acquisition module, an aircraft motion capture module and a data management module; the flight parameter acquisition module comprises an inclination angle detection sensor, a photosensitive detection device and a laser capture device, and the aircraft motion capture module comprises an optical image capture analysis module and an infrared capture module; the data management module comprises a processor, a first storage device and a second storage device, wherein the first storage device and the second storage device are respectively connected with the processor; the processor is provided with a data test socket;
the data acquisition device comprises a miniature shell and a PCB (printed Circuit Board) arranged in the miniature shell, wherein one end of the miniature shell is provided with a plug-in port used for being fixedly connected to an aircraft, and the miniature shell is also provided with an anti-falling device.
2. The aircraft testing device capable of realizing man-machine real-time interaction as claimed in claim 1, wherein the anti-drop device is a magnetic attraction sheet, the magnetic attraction sheet is arranged on the upper surface of the micro-housing, and the magnetic attraction sheet is correspondingly connected with a magnetic attraction patch on the aircraft.
3. The aircraft testing device capable of realizing human-computer real-time interaction as claimed in claim 1, wherein the socket comprises a USB interface.
4. The aircraft testing device capable of realizing human-computer real-time interaction as claimed in claim 1, wherein an anti-release lock catch is arranged at the edge of the insertion port, embedded in the insertion groove of the aircraft and buckled with the edge of the insertion groove to realize locking.
5. The aircraft testing device capable of realizing man-machine real-time interaction as claimed in claim 1, wherein the data acquisition device comprises a gyroscope, an acceleration sensor and a data memory, the gyroscope and the acceleration sensor are respectively connected with the processor, and the processor is further data-interconnected with the data memory.
6. The aircraft testing device capable of realizing human-computer real-time interaction of claim 1, wherein the data acquisition device comprises a wireless transmission module, and the wireless transmission module comprises a 5G/4G/3G module, a Bluetooth module or a WIFI communication module.
7. The aircraft testing device capable of realizing man-machine real-time interaction as claimed in claim 1, wherein the control host is provided with a control handle, and the control handle sends a control command to the testing device main body through a network.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910931306.1A CN110697074A (en) | 2019-09-29 | 2019-09-29 | Aircraft testing device capable of realizing human-computer real-time interaction |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910931306.1A CN110697074A (en) | 2019-09-29 | 2019-09-29 | Aircraft testing device capable of realizing human-computer real-time interaction |
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| CN107357314A (en) * | 2017-08-30 | 2017-11-17 | 上海拓攻机器人有限公司 | A kind of unmanned vehicle long-range control method and system |
| CN107817405A (en) * | 2017-12-10 | 2018-03-20 | 西北农林科技大学 | A kind of electronic unmanned plane real-time energy efficiency data acquisition and track record device |
| CN207346123U (en) * | 2017-09-12 | 2018-05-11 | 四川海特高新技术股份有限公司 | A kind of testboard for the test of airplane data acquisition component |
| CN207510742U (en) * | 2017-11-06 | 2018-06-19 | 中航通飞华南飞机工业有限公司 | A kind of parameter acquisition and monitoring device for big flight control system performance test |
| CN108803633A (en) * | 2018-07-25 | 2018-11-13 | 安康学院 | A kind of unmanned plane low latitude monitoring system based on mobile communications network |
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2019
- 2019-09-29 CN CN201910931306.1A patent/CN110697074A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130289924A1 (en) * | 2012-04-27 | 2013-10-31 | Labthink Instruments Co., Ltd. | Plastic packaging materials testing system based on internet of things and cloud technology |
| CN107147710A (en) * | 2017-05-04 | 2017-09-08 | 众芯汉创（北京）科技有限公司 | A kind of power network unmanned plane inspection management control device |
| CN107357314A (en) * | 2017-08-30 | 2017-11-17 | 上海拓攻机器人有限公司 | A kind of unmanned vehicle long-range control method and system |
| CN207346123U (en) * | 2017-09-12 | 2018-05-11 | 四川海特高新技术股份有限公司 | A kind of testboard for the test of airplane data acquisition component |
| CN207510742U (en) * | 2017-11-06 | 2018-06-19 | 中航通飞华南飞机工业有限公司 | A kind of parameter acquisition and monitoring device for big flight control system performance test |
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| CN108803633A (en) * | 2018-07-25 | 2018-11-13 | 安康学院 | A kind of unmanned plane low latitude monitoring system based on mobile communications network |
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Application publication date: 20200117 |