CN115027686A - Novel wing control system of large unmanned aerial vehicle - Google Patents
Novel wing control system of large unmanned aerial vehicle Download PDFInfo
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- CN115027686A CN115027686A CN202210834833.2A CN202210834833A CN115027686A CN 115027686 A CN115027686 A CN 115027686A CN 202210834833 A CN202210834833 A CN 202210834833A CN 115027686 A CN115027686 A CN 115027686A
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- 238000004891 communication Methods 0.000 claims abstract description 25
- 238000012544 monitoring process Methods 0.000 claims abstract description 20
- 238000007405 data analysis Methods 0.000 claims abstract description 16
- 238000006243 chemical reaction Methods 0.000 claims description 9
- 230000008602 contraction Effects 0.000 claims description 6
- 230000004927 fusion Effects 0.000 claims description 6
- 230000002265 prevention Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
- H04W4/30—Services specially adapted for particular environments, situations or purposes
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses a novel wing control system of a large unmanned aerial vehicle, which comprises a monitoring end and a control end, wherein the monitoring end comprises a monitoring unit, a monitoring data analysis unit and a first wireless communication unit, and the control end comprises a second wireless communication unit, a server, an early warning unit and a wing control unit. This novel wing control system of large-scale unmanned aerial vehicle, through wing the settlement of control unit, the user can make the wing shrink or wing slope according to the feedback, makes things convenient for large-scale unmanned aerial vehicle to get into constrictive environment, through the cooperation of monitor cell, control data analysis unit and early warning unit, makes the control prevention to unmanned aerial vehicle operating condition, greatly reduced the probability that the incident takes place.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle wing control, in particular to a novel wing control system of a large unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
The existing wing control of the large unmanned aerial vehicle is usually to control the direction and the rotating speed of the wing, but when meeting narrow environment, the large unmanned aerial vehicle can not pass through completely, and the wing working state of the large unmanned aerial vehicle is lack of monitoring and early warning, so that safety accidents are easily caused.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides a novel wing control system of a large unmanned aerial vehicle, which solves the problem.
(II) technical scheme
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides a novel wing control system of large-scale unmanned aerial vehicle, includes control end and control end, the control end includes monitoring unit, control data analysis unit and first wireless communication unit, the control end includes second wireless communication unit, server, early warning unit and wing control unit, monitoring unit's output and monitoring data analysis unit's input are connected, and monitoring data analysis unit's output and first wireless communication unit's input are connected, first wireless communication unit's output and monitoring unit's input are connected, and first wireless communication unit realizes both way junction with the second wireless communication unit, second wireless communication unit realizes both way junction with the server, the server realizes both way junction with the early warning unit, and the server realizes both way junction with the wing control unit.
Preferably, the monitoring unit comprises a wing inclination angle measuring module, a motor working state measuring module, a height measuring module and a GPS module.
Preferably, the monitoring data analysis unit includes a data classification module, a data conversion module and a data fusion module, an output end of the data classification module is connected with an input end of the data conversion module, and an output end of the data conversion module is connected with an input end of the data fusion module.
Preferably, the early warning unit comprises a comparison data setting module, a data comparison module and an alarm feedback module, wherein the output end of the comparison data setting module is connected with the input end of the data comparison module, and the output end of the data comparison module is connected with the input end of the alarm feedback module.
Preferably, the wing control unit includes wing shrink module, wing slope module and display module, wing shrink module includes electric putter and rotor motor, wing slope module includes servo motor, the display module includes touch module and button module.
(III) advantageous effects
The invention provides a novel wing control system of a large unmanned aerial vehicle. Compared with the prior art, the method has the following beneficial effects:
(1) this novel wing control system of large-scale unmanned aerial vehicle, through wing the settlement of control unit, the user can make the wing shrink or wing slope according to the feedback, makes things convenient for large-scale unmanned aerial vehicle to get into constrictive environment, through the cooperation of monitor cell, control data analysis unit and early warning unit, makes the control prevention to unmanned aerial vehicle operating condition, greatly reduced the probability that the incident takes place.
Drawings
FIG. 1 is a schematic block diagram of the system of the present invention;
FIG. 2 is a schematic block diagram of a monitoring unit of the present invention;
FIG. 3 is a schematic block diagram of a monitoring data analysis unit of the present invention;
fig. 4 is a schematic block diagram of the early warning unit of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, an embodiment of the present invention provides a technical solution: the utility model provides a novel wing control system of large-scale unmanned aerial vehicle, including control end and control end, the control end includes the control unit, control data analysis unit and first wireless communication unit, the control end includes the second wireless communication unit, the server, early warning unit and wing control unit, the output of control unit is connected with the input of control data analysis unit, and the output of control data analysis unit is connected with the input of first wireless communication unit, the output of first wireless communication unit is connected with the input of control unit, and first wireless communication unit realizes two-way junction with the second wireless communication unit, the second wireless communication unit realizes two-way junction with the server, the server realizes two-way junction with early warning unit, and the server realizes two-way junction with the wing control unit, the control unit includes wing inclination measuring module, motor operating condition measuring module, The monitoring data analysis unit comprises a data classification module, a data conversion module and a data fusion module, the output end of the data classification module is connected with the input end of the data conversion module, the output end of the data conversion module is connected with the input end of the data fusion module, the early warning unit comprises a comparison data setting module, a data comparison module and an alarm feedback module, the output end of the comparison data setting module is connected with the input end of the data comparison module, the output end of the data comparison module is connected with the input end of the alarm feedback module, the wing control unit comprises a wing contraction module, a wing inclination module and a display module, the wing contraction module comprises an electric push rod and a rotor motor, the wing inclination module comprises a servo motor, the display module comprises a touch control module and a key module, and a user can make wing contraction or wing inclination according to feedback through the setting of the wing control unit, make things convenient for large-scale unmanned aerial vehicle to get into constrictive environment, through the cooperation of monitoring unit, control data analysis unit and early warning unit, make the control prevention to unmanned aerial vehicle operating condition, greatly reduced the probability that the incident takes place.
And those not described in detail in this specification are well within the skill of those in the art.
Principle of operation
When the unmanned aerial vehicle flies, a wing inclination angle measuring module of the monitoring unit, a motor working state measuring module, a height measuring module and a GPS module respectively measure a wing inclination angle, a motor working state and a flying height, the GPS module positions the unmanned aerial vehicle and then transmits data to a monitoring data analyzing unit, the data classifying module classifies the data, the data converting module converts the data, the data fusing module fuses a plurality of groups of data, the data are transmitted to a second wireless communication unit through a first wireless communication unit, the second wireless communication unit transmits the data to a server, and the server transmits the data to an early warning unit and a wing control unit;
the data comparison module in the early warning unit compares the received data with the data set by the data setting module, if the received data is higher than the set value, the alarm feedback module gives an alarm, and if the received data is lower than the set value or gives an alarm, the alarm feedback module transmits information back to the server, the wing control unit receives the data and then feeds the data back to the display module, and a user can make wing contraction or wing inclination according to the feedback.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides a novel wing control system of large-scale unmanned aerial vehicle, includes control end and control end, its characterized in that: the control end includes second wireless communication unit, server, early warning unit and wing the control unit, the output of control unit is connected with the input of control data analysis unit, and the output of control data analysis unit is connected with first wireless communication unit's input, first wireless communication unit's output is connected with the input of control unit, and first wireless communication unit realizes both way junction with the second wireless communication unit, the second wireless communication unit realizes both way junction with the server, the server realizes both way junction with the early warning unit, and server and wing the control unit realize both way junction.
2. The novel wing control system of large unmanned aerial vehicle of claim 1, characterized in that: the monitoring unit comprises a wing inclination angle measuring module, a motor working state measuring module, a height measuring module and a GPS module.
3. The novel wing control system of large unmanned aerial vehicle of claim 1, characterized in that: the monitoring data analysis unit comprises a data classification module, a data conversion module and a data fusion module, wherein the output end of the data classification module is connected with the input end of the data conversion module, and the output end of the data conversion module is connected with the input end of the data fusion module.
4. The novel wing control system of large unmanned aerial vehicle of claim 1, characterized in that: the early warning unit comprises a comparison data setting module, a data comparison module and an alarm feedback module, wherein the output end of the comparison data setting module is connected with the input end of the data comparison module, and the output end of the data comparison module is connected with the input end of the alarm feedback module.
5. The novel wing control system of large unmanned aerial vehicle of claim 1, characterized in that: the wing control unit comprises a wing contraction module, a wing inclination module and a display module, the wing contraction module comprises an electric push rod and a rotor motor, the wing inclination module comprises a servo motor, and the display module comprises a touch module and a button module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210834833.2A CN115027686A (en) | 2022-07-15 | 2022-07-15 | Novel wing control system of large unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210834833.2A CN115027686A (en) | 2022-07-15 | 2022-07-15 | Novel wing control system of large unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN115027686A true CN115027686A (en) | 2022-09-09 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210834833.2A Pending CN115027686A (en) | 2022-07-15 | 2022-07-15 | Novel wing control system of large unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115027686A (en) |
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2022
- 2022-07-15 CN CN202210834833.2A patent/CN115027686A/en active Pending
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