CN110641730A - Full-freedom-degree miniature aircraft test platform - Google Patents
Full-freedom-degree miniature aircraft test platform Download PDFInfo
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- CN110641730A CN110641730A CN201910921126.5A CN201910921126A CN110641730A CN 110641730 A CN110641730 A CN 110641730A CN 201910921126 A CN201910921126 A CN 201910921126A CN 110641730 A CN110641730 A CN 110641730A
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- 238000012360 testing method Methods 0.000 title claims abstract description 79
- 238000013500 data storage Methods 0.000 claims abstract description 5
- 230000005540 biological transmission Effects 0.000 claims description 8
- 230000002159 abnormal effect Effects 0.000 claims description 3
- 230000001133 acceleration Effects 0.000 claims description 3
- 238000001914 filtration Methods 0.000 claims description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
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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 a full-freedom-degree miniature aircraft test platform which is characterized by comprising a mobile test main body, a data transmitting main body and a remote control operation handle, wherein the mobile test main body is respectively connected with the data transmitting main body and an aircraft through a wireless network; the mobile test main body comprises a wireless communication unit, a data storage unit, a distance positioning unit, an early warning unit, a data processing unit and a control unit, and the data transmitting main body comprises an ultrasonic transmitting unit, a wireless network unit, a micro sensing unit and a storage unit. The mobile test body is small in size, is inserted into the aircraft, collects data of the aircraft in real time, and transmits the data to the data transmitting body, so that the test on the real environment of the aircraft is facilitated.
Description
Technical Field
The invention relates to the field of aircraft testing, in particular to a full-freedom-degree miniature aircraft testing platform.
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 a full-freedom-degree miniature aircraft test platform which comprises a mobile test main body, a data transmitting main body and a remote control operation handle, wherein the motion of an aircraft can be operated in real time through the remote control operation handle, and the mobile test main body is small in size, is inserted into the aircraft, acquires data of the aircraft in real time and transmits the data to the data transmitting main body, so that the test of the real environment of the aircraft is facilitated.
The purpose of the invention is realized by the following technical scheme:
a full-freedom-degree miniature aircraft test platform comprises a mobile test main body, a data transmitting main body and a remote control operation handle, wherein the mobile test main body is respectively connected with the data transmitting main body and an aircraft through a wireless network; the mobile test main body comprises a wireless communication unit, a data storage unit, a distance positioning unit, an early warning unit, a data processing unit and a control unit, and the data transmitting main body comprises an ultrasonic transmitting unit, a wireless network unit, a micro sensing unit and a storage unit;
the wireless communication unit is used for being interconnected with the data transmission main body through a wireless network;
the distance positioning unit comprises an ultrasonic receiving device, and the ultrasonic receiving device calculates the current distance of the aircraft according to the time for receiving ultrasonic waves;
the early warning unit comprises an acousto-optic early warning device, and the early warning device is used for early warning an abnormal flight state;
the data processing unit is used for amplifying and filtering the received data and sending the processed data to the control unit for analysis;
the control unit is used for acquiring data information of the aircraft, analyzing and judging according to the acquired data information, and automatically generating a data test table;
the ultrasonic transmitting unit comprises an ultrasonic transmitting device, the ultrasonic transmitting device is used for transmitting an ultrasonic signal to the ultrasonic receiving device and transmitting a time node for transmitting ultrasonic waves to the mobile test main body through a wireless network;
the wireless network unit is used for establishing a wireless data communication channel with the mobile test main body;
the micro sensor comprises a plurality of sensors and is used for collecting flight data information of the aircraft, and the flight data information comprises acceleration, inclination angle and instantaneous speed information.
Furthermore, the mobile test main body is of a rectangular structure, a rechargeable battery is arranged in the mobile test main body, a wireless charging panel is arranged on the upper surface of the mobile test main body, and the wireless charging panel is electrically connected with the rechargeable battery through a conducting wire.
Furthermore, a plurality of data plug connectors are arranged on the upper side face of the movable testing main body.
Furthermore, the data transmission main body is of a flat rectangular structure, and a USB plug is arranged at the front end of the data transmission main body.
Furthermore, the remote control operation handle comprises a display screen, and an alarm lamp is arranged on one side of the display screen.
The invention has the beneficial effects that:
(1) the mobile test body is small in size, is inserted into the aircraft, collects data of the aircraft in real time, and transmits the data to the data transmitting body, so that the real environment of the aircraft can be tested;
(2) the distance between the aircraft and the data transmitting main body can be measured through ultrasonic waves, short-distance positioning and aircraft test control are facilitated, and the problem that test data errors are overlarge due to the fact that the aircraft height and the space environment influence is avoided.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a block diagram of the module connections of the mobile test agent of the present invention;
in the figure, 10-a data transmitting body, 11-a remote control operation handle, 12-a mobile testing body, 21-a control unit, 22-a wireless communication unit, 23-a data storage unit, 24-a distance positioning unit, 25-an early warning unit and 26-a data processing unit.
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 a full-freedom-degree miniature aircraft test platform, which is shown in fig. 1 and fig. 2 and comprises a mobile test main body 12, a data transmitting main body 10 and a remote control operation handle 11, wherein the mobile test main body 12 is respectively connected with the data transmitting main body 10 and an aircraft through a wireless network, and the mobile test main body 12 and the aircraft are also connected with the remote control operation handle 11 through a wireless network; the mobile test main body 12 comprises a wireless communication unit 22, a data storage unit 23, a distance positioning unit 24, an early warning unit 25, a data processing unit 26 and a control unit 21, and the data transmitting main body comprises an ultrasonic transmitting unit, a wireless network unit, a micro sensing unit and a storage unit;
the wireless communication unit 22 is used for data interconnection with a data transmitting main body through a wireless network;
the distance positioning unit 24 comprises an ultrasonic receiving device which calculates the current distance of the aircraft according to the time for receiving the ultrasonic waves;
the early warning unit 25 comprises an acousto-optic early warning device, and the early warning device is used for early warning an abnormal flight state;
the data processing unit 26 is configured to amplify and filter the received data, and send the processed data to the control unit for analysis;
the control unit 21 is configured to obtain data information of the aircraft, perform analysis and judgment according to the obtained data information, and automatically generate a data test table;
the ultrasonic transmitting unit comprises an ultrasonic transmitting device, the ultrasonic transmitting device is used for transmitting an ultrasonic signal to the ultrasonic receiving device and transmitting a time node for transmitting ultrasonic waves to the mobile test main body through a wireless network;
the wireless network unit is used for establishing a wireless data communication channel with the mobile test main body;
the micro sensor comprises a plurality of sensors and is used for collecting flight data information of the aircraft, and the flight data information comprises acceleration, inclination angle and instantaneous speed information.
The embodiment comprises a mobile test main body 12, a data transmitting main body 10 and a remote control operation handle 11, the motion of the aircraft can be operated in real time through the remote control operation handle 11, and the mobile test main body 12 is inserted into the aircraft due to small size, collects data of the aircraft in real time and transmits the data to the data transmitting main body 10, so that the test on the real environment of the aircraft is facilitated.
Example 2:
this embodiment is on embodiment 1's basis, it is the cuboid structure to remove test subject 12, be equipped with rechargeable battery in the removal test subject 12, it is equipped with wireless charging panel to remove test subject 12 upper surface, wireless charging panel passes through the wire and is connected with rechargeable battery electricity, it is equipped with a plurality of data connector to remove the side on test subject 12, data transmission subject 10 is flat rectangle structure, the front end of data transmission subject is equipped with the USB connector, remote control handle 11 includes the display screen, display screen one side is equipped with the alarm lamp.
The mobile test body 12 is of a flat rectangular structure and is convenient to be inserted into an aircraft. The mobile test subject 12 can acquire data of the aircraft in real time and feed the aircraft back to the test platform, etc.
The device comprises a mobile test main body 12, a data transmitting main body 10 and a remote control operation handle 11, the motion of the aircraft can be operated in real time through the remote control operation handle 11, and the mobile test main body 12 is small in size, is inserted into the aircraft, acquires data of the aircraft in real time and transmits the data to the data transmitting main body, so that the real environment of the aircraft can be tested; the distance between the aircraft and the data transmitting main body can be measured through ultrasonic waves, short-distance positioning and aircraft test control are facilitated, and the problem that test data errors are overlarge due to the fact that the aircraft height and the space environment influence is avoided.
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 (5)
1. A full-freedom-degree miniature aircraft test platform is characterized by comprising a mobile test main body, a data transmitting main body and a remote control operation handle, wherein the mobile test main body is respectively connected with the data transmitting main body and an aircraft through a wireless network; the mobile test main body comprises a wireless communication unit, a data storage unit, a distance positioning unit, an early warning unit, a data processing unit and a control unit, and the data transmitting main body comprises an ultrasonic transmitting unit, a wireless network unit, a micro sensing unit and a storage unit;
the wireless communication unit is used for being interconnected with the data transmission main body through a wireless network;
the distance positioning unit comprises an ultrasonic receiving device, and the ultrasonic receiving device calculates the current distance of the aircraft according to the time for receiving ultrasonic waves;
the early warning unit comprises an acousto-optic early warning device, and the early warning device is used for early warning an abnormal flight state;
the data processing unit is used for amplifying and filtering the received data and sending the processed data to the control unit for analysis;
the control unit is used for acquiring data information of the aircraft, analyzing and judging according to the acquired data information, and automatically generating a data test table;
the ultrasonic transmitting unit comprises an ultrasonic transmitting device, the ultrasonic transmitting device is used for transmitting an ultrasonic signal to the ultrasonic receiving device and transmitting a time node for transmitting ultrasonic waves to the mobile test main body through a wireless network;
the wireless network unit is used for establishing a wireless data communication channel with the mobile test main body;
the micro sensor comprises a plurality of sensors and is used for collecting flight data information of the aircraft, and the flight data information comprises acceleration, inclination angle and instantaneous speed information.
2. The full-freedom test platform for the micro aircraft as claimed in claim 1, wherein the movable test body is a rectangular structure, the movable test body is provided with a rechargeable battery therein, the upper surface of the movable test body is provided with a wireless charging plate, and the wireless charging plate is electrically connected with the rechargeable battery through a conducting wire.
3. The full-freedom test platform for micro aircrafts as recited in claim 1, wherein the upper side of the mobile test body is provided with a plurality of data plugs.
4. The full-freedom micro aircraft test platform according to claim 1, wherein the data transmission body is of a flat rectangular structure, and a USB plug is arranged at the front end of the data transmission body.
5. The full-freedom test platform for the micro aircraft as claimed in claim 1, wherein the remote control operation handle comprises a display screen, and an alarm lamp is arranged on one side of the display screen.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910921126.5A CN110641730A (en) | 2019-09-27 | 2019-09-27 | Full-freedom-degree miniature aircraft test platform |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910921126.5A CN110641730A (en) | 2019-09-27 | 2019-09-27 | Full-freedom-degree miniature aircraft test platform |
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| CN110641730A true CN110641730A (en) | 2020-01-03 |
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| CN201910921126.5A Pending CN110641730A (en) | 2019-09-27 | 2019-09-27 | Full-freedom-degree miniature aircraft test platform |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101448338A (en) * | 2008-11-27 | 2009-06-03 | 北京理工大学 | Mobile three-dimensional spatial wireless testing network system |
| CN102830691A (en) * | 2012-07-20 | 2012-12-19 | 南京航空航天大学 | Automatic detecting and fault diagnosing method of unmanned aerial vehicle based on cloud computing |
| CN105739516A (en) * | 2016-05-09 | 2016-07-06 | 王彦成 | Unmanned plane management and control device and corresponding system |
| 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 |
| US20180210441A1 (en) * | 2017-01-24 | 2018-07-26 | National Taiwan University | Uav, control system and intermediary device for uav |
| CN108391278A (en) * | 2018-01-31 | 2018-08-10 | 北京电子工程总体研究所 | The test analysis of aerocraft system based on 4G networks and diagnostic system and method |
-
2019
- 2019-09-27 CN CN201910921126.5A patent/CN110641730A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101448338A (en) * | 2008-11-27 | 2009-06-03 | 北京理工大学 | Mobile three-dimensional spatial wireless testing network system |
| CN102830691A (en) * | 2012-07-20 | 2012-12-19 | 南京航空航天大学 | Automatic detecting and fault diagnosing method of unmanned aerial vehicle based on cloud computing |
| CN105739516A (en) * | 2016-05-09 | 2016-07-06 | 王彦成 | Unmanned plane management and control device and corresponding system |
| US20180210441A1 (en) * | 2017-01-24 | 2018-07-26 | National Taiwan University | Uav, control system and intermediary device for uav |
| 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 |
| CN108391278A (en) * | 2018-01-31 | 2018-08-10 | 北京电子工程总体研究所 | The test analysis of aerocraft system based on 4G networks and diagnostic system and method |
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