CN106681360B - Multi-rotor unmanned aerial vehicle with high-brightness aerial illumination - Google Patents
Multi-rotor unmanned aerial vehicle with high-brightness aerial illumination Download PDFInfo
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- CN106681360B CN106681360B CN201710168921.2A CN201710168921A CN106681360B CN 106681360 B CN106681360 B CN 106681360B CN 201710168921 A CN201710168921 A CN 201710168921A CN 106681360 B CN106681360 B CN 106681360B
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 11
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
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Abstract
The invention discloses a multi-rotor unmanned aerial vehicle with high-brightness aerial illumination, which comprises a mobile end and a terminal, wherein the mobile end is arranged on the multi-rotor unmanned aerial vehicle, and the terminal is arranged in a ground receiving station; the mobile terminal comprises a mobile terminal central processing unit, a mobile terminal data transmission module, a mobile terminal remote control receiver module, a mobile terminal LED lamp power supply control module and a mobile terminal LED lamp; the mobile terminal central processing unit is respectively connected with the mobile terminal data transmission module, the mobile terminal remote control receiver module and the mobile terminal LED lamp power supply control module; the terminal comprises a terminal data transmission module and a terminal aircraft remote controller which are respectively connected with the terminal central processing unit and are in bidirectional communication; the mobile terminal remote control receiver module receives signals sent by the terminal aircraft remote controller, and the mobile terminal LED lamp switch control is realized through the mobile terminal LED lamp power supply control module. The invention solves the defect of the existing multi-rotor unmanned aerial vehicle in field command and regulation application through airborne high-brightness aerial illumination.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a multi-rotor unmanned aerial vehicle with a high-brightness aerial lighting function.
Background
The rotor unmanned aerial vehicle is an advanced vertical take-off and landing micro automatic piloting unmanned aerial vehicle system, is suitable for departments such as fire control, traffic, police technical detection and the like, can take off and land in all terrain, carries task loads and is used for executing various air tasks such as target reconnaissance, tracking, real-time information collection and the like.
The unmanned aerial vehicle has the advantages of small size, flexibility, simplicity in operation, convenience in maintenance, convenience in carrying, high reliability, high cost performance and the like, and in addition, the unmanned aerial vehicle has all-terrain take-off and landing capability and high intelligence, can fly in various postures, such as hovering, forward flying, side flying, back flying and the like, and has special use value which is difficult to compare with that of a fixed-wing unmanned aerial vehicle.
For public services, the role of the drone is also great. For example, in the aspect of urban traffic, road information conditions are processed by means of road cameras, various data are required to be processed, and an unmanned aerial vehicle can collect data of the whole congestion area, so that traffic departments can formulate evacuation schemes in a targeted manner, and the problem of congestion is solved. Traffic data collected in the traditional mode is scattered, and effective data statistics effect is difficult to form. The satellite is high in cost, the precision of the satellite cannot be compared with that of an unmanned aerial vehicle which is truly close to the ground, and the unmanned aerial vehicle with the high-brightness air lighting function possibly has many applications in the traffic field, and the unmanned aerial vehicle has unique advantages in daily management of cities and emergency traffic conditions. However, at present, the multi-rotor unmanned aerial vehicle does not have the high-brightness aerial lighting function, and the defect of the multi-rotor unmanned aerial vehicle in field command and regulation application exists, so that the problem needs to be solved.
Disclosure of Invention
Aiming at the defects of the existing multi-rotor unmanned aerial vehicle in the aspects of fire control, traffic, police technical detection and the like, the invention provides the multi-rotor unmanned aerial vehicle with high-brightness air lighting, which has the advantages that the high-brightness LED lamp lighting function is added, the unmanned aerial vehicle can be started at night or in the light, the limitation of the insufficient light to the unmanned aerial vehicle flight is overcome, and meanwhile, the transaction processing efficiency is effectively improved.
The aim of the invention can be achieved by the following technical scheme:
the multi-rotor unmanned aerial vehicle with high-brightness air illumination comprises a mobile end and a terminal, wherein the mobile end is arranged on the multi-rotor unmanned aerial vehicle, and the terminal is arranged in a ground receiving station;
the mobile terminal comprises a mobile terminal central processing unit, a mobile terminal data transmission module, a mobile terminal remote control receiver module, a mobile terminal LED lamp power supply control module and a mobile terminal LED lamp; the mobile terminal central processing unit is respectively connected with the mobile terminal data transmission module, the mobile terminal remote control receiver module and the mobile terminal LED lamp power supply control module;
the terminal comprises a terminal data transmission module and a terminal aircraft remote controller which are respectively connected with the terminal central processing unit and are in bidirectional communication;
the mobile terminal remote control receiver module receives signals sent by the terminal aircraft remote controller, and the mobile terminal LED lamp switch control is realized through the mobile terminal LED lamp power supply control module.
The mobile terminal central processing unit receives command information sent by the ground station through the mobile terminal data transmission module, the terminal data transmission module and the terminal central processing unit.
The mobile terminal data transmission module is in bidirectional communication with the mobile terminal central processing unit, and the mobile terminal central processing unit receives information sent by the terminal and then performs corresponding operation.
And the mobile terminal central processor and the terminal central processor are in bidirectional communication through the mobile terminal data transmission module and the terminal data transmission module.
The movable end further comprises a movable end steering engine, the movable end steering engine is respectively connected to the movable end LED lamp power supply control module and the movable end LED lamp, and the movable end steering engine adjusts the pitching angle of the movable end LED lamp.
The movable end LED lamp comprises four LED strong lights and fixed radiating fins, and a fixed lens is arranged in front of the LED lamp.
The mobile terminal also comprises a flight control module and a cradle head control module; the control module is in bidirectional communication with the mobile terminal central processing unit, and the cradle head control module is used for receiving the control instruction of the mobile terminal central processing unit in one way.
And the mobile terminal central processing unit of the mobile terminal analyzes the received command information and sends the command information to the flight control module or the cradle head control module, so that the multi-rotor unmanned aerial vehicle completes corresponding flight actions and the cradle head completes corresponding actions.
The model of the flight control module is Pixhawkk 2.4.6; the model of the mobile terminal central processing unit is STM32F103RCT6; the model of the cradle head control module is A5W-K.
The model of the mobile terminal data transmission module is Xtend900MHz; the model of the power supply control module of the LED lamp at the mobile end is JS-2000B; the model of the LED lamp at the mobile end is JSELED_4; the terminal central processing unit model is STM32F103RCT6; the model of the terminal data transmission module is Xtend900MHz.
The invention has the beneficial effects that:
1. according to the invention, through the power supply control module of the LED lamp at the mobile end, the LED lamp at the mobile end can be switched on and off in real time in the air, so that the mobile LED lamp has high flexibility;
2. the pitching angle of the whole LED lamp structure can be adjusted by the movable end LED lamp through the movable end steering engine, so that the angle of lamplight illumination can be adjusted; in addition, a fixed lens is arranged in front of the LED lamp, and the function of adjusting the focal length can be achieved by adjusting the distance between the LED lamp and the lens, so that the optimal effect of air illumination is achieved;
3. an ultra-long distance data transmission module is adopted, so that the transmission distance of data is effectively ensured;
4. the LED lamp power supply adopts an independent voltage stabilizing module, so that the stability is good;
5. the power supply adopted by the invention has wide range and good applicability;
6. according to the invention, the pitching of the camera is controlled by the cradle head, so that the shooting range is effectively increased, and the shooting target can be effectively locked;
7. according to the invention, high-brightness aerial illumination can be carried out on special areas such as dangerous areas, bad weather, insufficient brightness, night rescue and the like through airborne high-brightness aerial illumination, so that quick positioning, target determination and data acquisition are realized, on-site commanders are effectively helped to accurately grasp on-site conditions, basis is provided for scientific decision making, the current environment condition is displayed in real time through installing the high-brightness aerial illumination on the unmanned aerial vehicle, the transaction processing efficiency is improved more effectively, and the defects of the existing multi-rotor unmanned aerial vehicle in on-site command and regulation application are overcome;
8. according to the high-brightness LED lamp lighting function of the unmanned aerial vehicle, the unmanned aerial vehicle can fly normally at night, and road condition information at night is collected.
Drawings
The present invention is further described below with reference to the accompanying drawings for the convenience of understanding by those skilled in the art.
Fig. 1 is a schematic diagram of the structure of the present invention.
Detailed Description
The structural features of the present invention will now be described in detail with reference to the accompanying drawings.
A multi-rotor unmanned aerial vehicle with high-brightness air lighting, see fig. 1, comprises a mobile terminal 10 and a terminal 20, wherein the mobile terminal 10 is installed on the multi-rotor unmanned aerial vehicle, and the terminal 20 is installed in a ground receiving station;
the mobile terminal 10 comprises a mobile terminal central processing unit 11, a mobile terminal data transmission module 12, a mobile terminal remote control receiver module 13, a mobile terminal LED lamp power supply control module 14, a mobile terminal LED lamp 15 and a mobile terminal steering engine 16; specifically, the mobile terminal central processing unit 11 is respectively connected with the mobile terminal data transmission module 12, the mobile terminal remote control receiver module 13 and the mobile terminal LED lamp power supply control module 14; the mobile terminal data transmission module 12 is in bidirectional communication with the mobile terminal central processing unit 11, receives information sent by the terminal 20, and the mobile terminal central processing unit 11 processes the received signal to the mobile terminal LED lamp power supply control module 14 to control the switching of the mobile terminal LED lamp 15;
the terminal 20 comprises a terminal central processing unit 21, a terminal data transmission module 22 and a terminal airplane remote controller 23; specifically, the terminal data transmission module 22 and the terminal aircraft remote controller 23 are respectively connected with the terminal central processing unit 21 and are in bidirectional communication;
the mobile terminal central processing unit 11 and the terminal central processing unit 21 are in bidirectional communication through the mobile terminal data transmission module 12 and the terminal data transmission module 22; the mobile terminal central processing unit 11 receives the information sent by the terminal 20 and then makes corresponding operation; the mobile terminal LED lamp power supply control module 14 receives a signal sent by the terminal aircraft remote controller 23 through the mobile terminal remote control receiver module 13 to control the on and off of the mobile LED lamp 15;
further, the power control module 14 of the mobile terminal LED lamp receives the signal sent by the remote control 23 of the terminal aircraft, and turns on and off the mobile terminal LED lamp 15.
Further, the mobile terminal data transmission module 12 is connected with the mobile terminal central processing unit 11, and bidirectional communication is realized through the data transmission module; the upper surface of the movable end steering engine 16 is fixed on a carbon plate (the movable end steering engine is manually adjusted and controlled before flying), and the movable end LED lamp 15 can adjust the pitching angle of the whole movable end LED lamp 15 structure through the movable end steering engine 16, so that the angle for adjusting the lighting of the lamplight is achieved; the movable end LED lamp 15 comprises 4 LED strong lights and fixed radiating fins, the radiating fins are utilized to dissipate heat better, in addition, a fixed lens is arranged in front of the movable end LED lamp 15, and the function of adjusting the focal length can be achieved by adjusting the distance between the movable end LED lamp 15 and the lens, so that the best effect of air illumination is achieved.
Further, the mobile terminal 10 further includes a flight control module 17 and a pan/tilt control module 18; the flight control module 17 is in two-way communication with the mobile terminal central processing unit 11, and the cradle head control module 18 receives control instructions of the mobile terminal central processing unit 11 in one way.
Further, the model of the flight control module 17 is pixhawk2.4.6; the model of the mobile terminal central processing unit 11 is STM32F103RCT6; the model of the mobile terminal data transmission module 12 is Xtend900MHz; the model of the mobile terminal LED lamp power supply control module 14 is JS-2000B; the model of the mobile end LED lamp 15 is JSELED_4; the model of the mobile end steering engine 16 is JSTJ_1; the model of the cradle head control module 18 is A5W-K; the model of the terminal central processing unit 21 is STM32F103RCT6; the model of the terminal data transmission module 22 is Xtend900MHz;
further, the mobile terminal central processing unit 11 receives command information sent by the ground station through the mobile terminal data transmission module 12, the terminal data transmission module 22 and the terminal central processing unit 21; the mobile terminal central processing unit 11 analyzes the received command information and then sends the command information to the flight control module 17 or the cradle head control module 18, so that the multi-rotor unmanned aerial vehicle can complete corresponding flight actions and the cradle head can complete corresponding actions.
The invention sets up the strong light lighting system in the front end of the unmanned aerial vehicle, with the aerial monitoring camera in the same direction setting. The unmanned aerial vehicle is used for carrying out high-brightness aerial illumination on special areas such as dangerous areas, bad climates, insufficient brightness, night rescue and the like, so that quick positioning, target determination and data acquisition are realized, the on-site commander is effectively helped to accurately master the on-site situation, and basis is provided for scientific decision making; the current environment condition is displayed in real time by installing high-brightness aerial illumination on the unmanned aerial vehicle, so that the efficiency of processing transactions is improved more effectively, and the defect of the existing multi-rotor unmanned aerial vehicle in field command and regulation application is overcome; the high-altitude illumination function is realized through the airborne strong illumination system, and the strong illumination system can be controlled to be turned on or off through the control terminal; the steering engine through the lighting system can adjust the lighting direction of the LED lamp at the mobile end, and is efficient and safe.
The foregoing is merely illustrative of the structures of this invention and various modifications, additions and substitutions for those skilled in the art can be made to the described embodiments without departing from the scope of the invention or from the scope of the invention as defined in the accompanying claims.
Claims (7)
1. The utility model provides a take many rotor unmanned aerial vehicle of high-brightness aerial illumination, includes removal end (10) and terminal (20), its characterized in that: the mobile terminal (10) is installed on the multi-rotor unmanned aerial vehicle, and the terminal (20) is installed in a ground receiving station;
the mobile terminal (10) comprises a mobile terminal central processing unit (11), a mobile terminal data transmission module (12), a mobile terminal remote control receiver module (13), a mobile terminal LED lamp power supply control module (14) and a mobile terminal LED lamp (15); the mobile terminal central processing unit (11) is respectively connected with the mobile terminal data transmission module (12), the mobile terminal remote control receiver module (13) and the mobile terminal LED lamp power supply control module (14);
the terminal (20) comprises a terminal data transmission module (22) and a terminal aircraft remote controller (23) which are respectively connected with the terminal central processing unit (21) and are in bidirectional communication;
the mobile terminal remote control receiver module (13) receives signals sent by the terminal aircraft remote controller (23), and the mobile terminal LED lamp (15) is controlled to be switched through the mobile terminal LED lamp power supply control module (14);
the movable end (10) further comprises a movable end steering engine (16), the movable end steering engine (16) is respectively connected to the movable end LED lamp power supply control module (14) and the movable end LED lamp (15), and the movable end steering engine (16) adjusts the pitching angle of the movable end LED lamp (15);
the movable end LED lamp (15) comprises four LED strong lights and fixed radiating fins, and a fixed lens is arranged in front of the LED lamp;
the mobile terminal (10) further comprises a flight control module (17) and a cradle head control module (18); the flight control module (17) is in bidirectional communication with the mobile terminal central processing unit (11), and the cradle head control module (18) is used for receiving control instructions of the mobile terminal central processing unit (11) in one direction.
2. The multi-rotor unmanned aerial vehicle with high-brightness air lighting of claim 1, wherein: the mobile terminal central processing unit (11) receives command information sent by the ground station through the mobile terminal data transmission module (12), the terminal data transmission module (22) and the terminal central processing unit (21).
3. The multi-rotor unmanned aerial vehicle with high-brightness air lighting according to claim 2, wherein: the mobile terminal data transmission module (12) is in bidirectional communication with the mobile terminal central processing unit (11), and the mobile terminal central processing unit (11) receives information sent by the terminal (20) and then performs corresponding operation.
4. A multi-rotor unmanned aerial vehicle with high brightness overhead lighting as claimed in claim 3, wherein: the mobile terminal central processing unit (11) and the terminal central processing unit (21) are in bidirectional communication through the mobile terminal data transmission module (12) and the terminal data transmission module (22).
5. The multi-rotor unmanned aerial vehicle with high-brightness air lighting of claim 1, wherein: the mobile terminal central processing unit (11) of the mobile terminal (10) analyzes the received command information and sends the command information to the flight control module (17) or the cradle head control module (18) so that the multi-rotor unmanned aerial vehicle can complete corresponding flight actions and the cradle head can complete corresponding actions.
6. The multi-rotor unmanned aerial vehicle with high-brightness air lighting of claim 1, wherein: the model of the flight control module (17) is Pixhawkk 2.4.6; the model of the mobile terminal central processing unit (11) is STM32F103RCT6; the model of the cradle head control module (18) is A5W-K.
7. The multi-rotor unmanned aerial vehicle with high-brightness air lighting of claim 1, wherein: the model of the mobile terminal data transmission module (12) is Xtend900MHz; the model of the mobile terminal LED lamp power supply control module (14) is JS-2000B; the model of the LED lamp (15) at the mobile end is JSELED_4; the terminal central processing unit (21) is STM32F103RCT6; the model of the terminal data transmission module (22) is Xtend900MHz.
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| CN201710168921.2A CN106681360B (en) | 2017-03-21 | 2017-03-21 | Multi-rotor unmanned aerial vehicle with high-brightness aerial illumination |
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| CN201710168921.2A CN106681360B (en) | 2017-03-21 | 2017-03-21 | Multi-rotor unmanned aerial vehicle with high-brightness aerial illumination |
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| CN106681360B true CN106681360B (en) | 2023-05-02 |
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| CN115309213B (en) * | 2022-04-20 | 2023-12-19 | 吴江高级中学 | Control method for biological experiment temperature and humidity control ecological environment box |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2817631A1 (en) * | 2000-12-05 | 2002-06-07 | Philippe Waquet | Remote control for aerial reconnaissance drone has section mounted in drone with computer and mobile telephone connection |
| CN104002978A (en) * | 2014-05-16 | 2014-08-27 | 哈尔滨工程大学 | Small searchlighting rotor flight vehicle |
| CN104483987A (en) * | 2014-12-29 | 2015-04-01 | 马鞍山市赛迪智能科技有限公司 | Drone airborne monitoring system |
| CN105346727A (en) * | 2015-10-30 | 2016-02-24 | 嘉兴亚欧光电科技有限公司 | Unmanned aerial vehicle carrying lighting lamp |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10051709B2 (en) * | 2013-12-17 | 2018-08-14 | Eaton Intelligent Power Limited | Selectable control for high intensity LED illumination system to maintain constant color temperature on a lit surface |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2817631A1 (en) * | 2000-12-05 | 2002-06-07 | Philippe Waquet | Remote control for aerial reconnaissance drone has section mounted in drone with computer and mobile telephone connection |
| CN104002978A (en) * | 2014-05-16 | 2014-08-27 | 哈尔滨工程大学 | Small searchlighting rotor flight vehicle |
| CN104483987A (en) * | 2014-12-29 | 2015-04-01 | 马鞍山市赛迪智能科技有限公司 | Drone airborne monitoring system |
| CN105346727A (en) * | 2015-10-30 | 2016-02-24 | 嘉兴亚欧光电科技有限公司 | Unmanned aerial vehicle carrying lighting lamp |
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