CN111924120A - Airborne monitoring control device and control method for unmanned aerial vehicle - Google Patents
Airborne monitoring control device and control method for unmanned aerial vehicle Download PDFInfo
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- 238000000034 method Methods 0.000 title claims abstract description 40
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- 229910001385 heavy metal Inorganic materials 0.000 claims description 3
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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
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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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
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Abstract
The invention discloses an airborne monitoring control device and a control method for an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. Including unmanned aerial vehicle, driving motor, screw, flight control master controller, support frame and machine carry the camera, the fixed driving motor that is provided with in unmanned aerial vehicle's top, driving motor's the fixed screw that is provided with of output shaft, unmanned aerial vehicle's the fixed tailstock that is provided with in rear side, the inside bottom of unmanned aerial vehicle is provided with flight control master controller and power supply battery, unmanned aerial vehicle's bottom is provided with the support frame. Utilize the airborne camera to carry out information acquisition, utilize the sensor unit to carry out data information acquisition, will obtain information transmission and give the flight control master controller of unmanned aerial vehicle inside, in-process unmanned aerial vehicle carries out the airborne monitoring control constantly and obtains positional information through the GPS module, can gather multiple information, information can in time collect the arrangement, fast carry out information display through showing control platform, reach better unmanned aerial vehicle airborne monitoring control's purpose.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an airborne monitoring control device and a control method of an unmanned aerial vehicle.
Background
Unmanned aircraft is called unmanned aerial vehicle for short, and is called UAV in short in English, and is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, compared with the unmanned aircraft, the unmanned aircraft is more suitable for tasks too 'fool, dirty or dangerous', the unmanned aircraft can be divided into military and civil according to the application field, and the unmanned aircraft can be divided into reconnaissance aircraft and target aircraft in the military, and the unmanned aircraft can be applied to the industry in the civil field, and is really just needed by the unmanned aircraft; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, the developed countries also actively expand the industrial application and the unmanned aerial vehicle technology, the unmanned aerial vehicle appears in the 20 th century at the earliest, the world war is going to be as well as the fire in 1914, the two general missions of Kadel and Pichel in the United kingdom propose a proposal to the military aviation society of military aviation in the United kingdom: the bold assumption of developing a small airplane that was operated by radio without human piloting, so that it could fly over a target area on the enemy, and dropped a bomb previously mounted on the small airplane, was immediately appreciated by the military aeronautical society of great britain, henderson jazz, at that time. He specified that he was developed by professor of a shift horse. Drones were used as targets for training at the time. Is a term used in many countries to describe the latest generation of unmanned aircraft. Literally, this term can describe cruise missiles that have evolved from kites, radio teleplanes, to V-1 missiles, but in military terms are limited to reusable heavier-than-air vehicles.
Along with the continuous development of social economy, unmanned aerial vehicle has obtained extensive use, unmanned aerial vehicle is at the aerial photograph at present, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, the relief of disaster, the film and television is shot, make the application in fields such as romantic, great expansion unmanned aerial vehicle's use itself, developed country is also in the active extension industry application and development unmanned aerial vehicle technique, the unmanned aerial vehicle monitoring control device that uses on the market at present is mostly simple function of shooing, the function is comparatively single, and unmanned aerial vehicle receives the damage easily in the use, for this, propose unmanned aerial vehicle machine carries monitoring control device and control method and solve above-mentioned problem.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an airborne monitoring control device and a control method of an unmanned aerial vehicle, and aims to solve the problems in the background art.
In order to achieve the purpose, the invention provides the following technical scheme: an airborne monitoring control device and a control method of an unmanned aerial vehicle comprise the unmanned aerial vehicle, a driving motor, propellers, a flight control main controller, a support frame and an airborne camera, wherein the driving motor is fixedly arranged at the top of the unmanned aerial vehicle, the propellers are fixedly arranged on an output shaft of the driving motor, a tail frame is fixedly arranged on the rear side of the unmanned aerial vehicle, the flight control main controller and a power supply battery are arranged at the bottom of the interior of the unmanned aerial vehicle, the support frame is arranged at the bottom of the unmanned aerial vehicle and comprises a fixed seat, a damping spring and a support plate, the support plate is arranged at the bottom of the fixed frame through the damping spring, and a;
an airborne camera is arranged on the front side of the bottom of the unmanned aerial vehicle and comprises a fixed rod, a movable shaft, a machine body and a camera head, the bottom of the fixed rod is movably provided with the machine body through the movable shaft, and the bottom of the machine body is fixedly provided with the camera head;
the output electricity of airborne camera and sensor unit is connected with the inside input that flies the accuse master controller of unmanned aerial vehicle, the output electricity that flies the accuse master controller is connected with driving motor and wireless communicator's input, the two-way electricity of output that flies the accuse master controller is connected with the input of GPS module, the input electricity that flies the accuse master controller is connected with the input of remote controller.
Further optimize this technical scheme, driving motor's output shaft is fixed and is provided with the pivot, and the fixed surface of pivot is provided with the connecting rod, and the one end that the pivot was kept away from to the connecting rod is provided with the screw through fixing bolt connection.
Further optimize this technical scheme, the fixed supplementary oar that is provided with in top of tailstock, the bottom of supplementary oar is provided with the motor.
Further optimize this technical scheme, the fixed fixing base that is provided with in bottom of support frame, the fixed damping spring that is provided with in bottom of fixing base, damping spring's the fixed backup pad that is provided with in bottom.
This technical scheme is further optimized, be connected the setting through the anchor strut between tailstock and the support frame, constitute the triangle setting between unmanned aerial vehicle, tailstock and the support frame.
Further optimize this technical scheme, organism and camera head can carry out the angle modulation of zero degree to one hundred twenty degrees under the effect of loose axle.
Further optimize this technical scheme, the output electricity of wireless communicator is connected with the input of display control platform, display control platform's inside is provided with display device.
Further optimize this technical scheme, the sensor unit includes heavy metal detector, smoke transducer, PM2.5 monitor and PM10 monitor.
An airborne monitoring control method of an unmanned aerial vehicle is characterized by comprising the following steps:
s1, sending an instruction to a flight control main controller inside the unmanned aerial vehicle by using a remote controller, controlling a driving motor to work by using the flight control main controller, and driving a propeller to rotate by using the rotation of the driving motor so that the unmanned aerial vehicle flies;
s2, acquiring information by using the airborne camera in the flying process, acquiring video and photo information, and transmitting the information acquired by the airborne camera to a flight control main controller in the unmanned aerial vehicle;
s3, acquiring data information by using the sensor unit in the flight process, and transmitting the acquired information to a flight control main controller in the unmanned aerial vehicle;
s4, after the flight control master controller obtains the information, the information is transmitted to the display control platform through the wireless communicator in time for information display, and meanwhile, the power supply battery supplies power in time;
s5, acquiring position information through the GPS module at all times when the unmanned aerial vehicle carries out airborne monitoring control in the flight process.
Further optimize this technical scheme, the model of flight control master controller is KY12S, the GPS module is the GPS locator, the GPS locator model is Air 800.
Compared with the prior art, the invention provides an airborne monitoring control device and a control method of an unmanned aerial vehicle, and the device and the method have the following beneficial effects:
1. according to the unmanned aerial vehicle airborne monitoring control device and the control method, an airborne camera is used for information acquisition, a sensor unit is used for data information acquisition, acquired information is transmitted to a flight control master controller inside the unmanned aerial vehicle, the unmanned aerial vehicle acquires position information through a GPS module at all times when airborne monitoring control is carried out in the flight process, various information can be acquired, the information can be collected and sorted in time, information display is carried out quickly through a display control platform, and the purpose of better unmanned aerial vehicle airborne monitoring control is achieved.
2. According to the airborne monitoring control device and the control method of the unmanned aerial vehicle, the damping mechanism is formed by matching the damping spring with the supporting plate at the bottom of the unmanned aerial vehicle, so that the unmanned aerial vehicle can be subjected to damping protection, the structure is simple, and the service life of the unmanned aerial vehicle can be prolonged.
3. According to the unmanned aerial vehicle airborne monitoring control device and the control method, the principle that the triangle arrangement is formed among the unmanned aerial vehicle, the tail frame and the support frame is beneficial to fully utilizing the stability of the triangle is formed, and therefore the unmanned aerial vehicle has better stability.
4. According to the unmanned aerial vehicle airborne monitoring control device and the control method, the angle of the machine body and the camera head can be adjusted according to actual needs, the regulation of the machine body and the camera head monitoring snapshot angle is facilitated, and further the use effect is improved.
Drawings
Fig. 1 is a schematic structural diagram of an airborne monitoring control device and a control method for an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of an airborne camera of an airborne monitoring control device and a control method of an unmanned aerial vehicle according to the present invention;
fig. 3 is an enlarged structural diagram of part a in fig. 1 of an airborne monitoring control device and a control method for an unmanned aerial vehicle according to the present invention;
fig. 4 is a control system diagram of an airborne monitoring control device and a control method for an unmanned aerial vehicle according to the present invention.
In the figure: 1. an unmanned aerial vehicle; 2. a drive motor; 3. a propeller; 4. a tailstock; 5. auxiliary propellers; 6. a flight control master controller; 7. a power supply battery; 8. a support frame; 81. a fixed seat; 82. a damping spring; 83. a support plate; 9. an onboard camera; 91. fixing the rod; 92. a movable shaft; 93. a body; 94. a camera head; 10. a sensor unit.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to 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.
Example (b):
referring to fig. 1-4, an airborne monitoring and controlling device for an unmanned aerial vehicle comprises an unmanned aerial vehicle 1, a driving motor 2, a propeller 3, a flight control master controller 6, a support frame 8 and an airborne camera 9, wherein the driving motor 2 is fixedly arranged at the top of the unmanned aerial vehicle 1, the propeller 3 is fixedly arranged on an output shaft of the driving motor 2, a tailstock 4 is fixedly arranged at the rear side of the unmanned aerial vehicle 1, the flight control master controller 6 and a power supply battery 7 are arranged at the bottom inside the unmanned aerial vehicle 1, the support frame 8 is arranged at the bottom of the unmanned aerial vehicle 1, the support frame 8 comprises a fixing seat 81, a damping spring 82 and a support plate 83, the support plate 83 is arranged at the bottom of the fixing frame 81 through the damping spring 82, a sensor unit 10 is arranged at the top inside the unmanned aerial vehicle 1, the airborne camera 9 comprises a fixed rod 91, a movable shaft 92, a body 93 and a camera head 94, the bottom of the fixed rod 91 is movably provided with the body 93 through the movable shaft 92, the bottom of the body 93 is fixedly provided with the camera head 94, the output ends of the airborne camera 9 and the sensor unit 10 are electrically connected with the input end of a flight control main controller 6 in the unmanned aerial vehicle 1, the output end of the flight control main controller 6 is electrically connected with a driving motor 2 and the input end of a wireless communicator, the output end of the flight control main controller 6 is electrically connected with the input end of a GPS module in a two-way manner, the input end of the flight control main controller 6 is electrically connected with the input end of a remote controller, the airborne camera 9 is used for information acquisition, the sensor unit 10 is used for data information acquisition, the acquired information is transmitted to the flight control main controller 6 in the unmanned aerial vehicle 1, and the, can gather multiple information, the information can in time collect the arrangement, carries out information display through showing control platform fast, reaches better unmanned aerial vehicle machine carries monitor control's purpose.
As the specific optimization scheme of this embodiment, the fixed pivot that is provided with of output shaft of driving motor 2, and the fixed surface of pivot is provided with the connecting rod, and the one end that the pivot was kept away from to the connecting rod is provided with screw 3 through fixing bolt connection, and screw 3 connects the setting through fixing bolt, and the screw 3 of being convenient for is installed and is dismantled and the periodic maintenance work, and this has improved staff's work efficiency greatly.
As the specific optimization scheme of this embodiment, the fixed supplementary oar 5 that is provided with in top of tailstock 4, the bottom of supplementary oar 5 is provided with the motor, and supplementary oar 5's setting can do benefit to unmanned aerial vehicle 1's balanced design, increases drive power when can flying again, does benefit to unmanned aerial vehicle 1's flight work.
As the specific optimization scheme of this embodiment, the fixed fixing base 81 that is provided with in bottom of support frame 8, the fixed damping spring 82 that is provided with in bottom of fixing base 81, the fixed backup pad 83 that is provided with in bottom of damping spring 82, pass through damping spring 82 cooperation backup pad 83 and constitute a damper in unmanned aerial vehicle 1's bottom, can carry out shock attenuation protection to unmanned aerial vehicle 1, do benefit to extension its life.
As the specific optimization scheme of this embodiment, be connected the setting through the anchor strut between tailstock 4 and the support frame 8, constitute the triangle setting between unmanned aerial vehicle 1, tailstock 4 and the support frame 8, the setting of anchor strut does benefit to the steadiness that increases this unmanned aerial vehicle 1, constitutes the triangle setting between unmanned aerial vehicle 1, tailstock 4 and the support frame 8 and does benefit to the principle of make full use of triangle-shaped stability, and then makes this unmanned aerial vehicle have better steadiness.
As a specific optimization scheme of this embodiment, the body 93 and the camera head 94 can be angularly adjusted from zero degrees to one hundred twenty degrees under the action of the movable shaft 92, and the body 93 and the camera head 94 can be angularly adjusted according to actual needs, so that the body 93 and the camera head 94 can be adjusted to monitor the snapshot angle, and the use effect is further improved.
As a specific optimization scheme of this embodiment, the output end of the wireless communicator is electrically connected to the input end of the display control platform, and the display device is arranged inside the display control platform.
As a specific optimization scheme of the embodiment, the sensor unit comprises a heavy metal detector, a smoke sensor, a PM2.5 monitor, and a PM10 monitor.
An airborne monitoring control method for an unmanned aerial vehicle comprises the following steps:
s1, sending an instruction to a flight control main controller 6 inside the unmanned aerial vehicle 1 by using a remote controller, controlling a driving motor 2 to work by using the flight control main controller 6, and driving a propeller 3 to rotate by using the rotation of the driving motor 2 so that the unmanned aerial vehicle 1 flies;
s2, in the flying process, the airborne camera 9 is used for collecting information, video and photo information is obtained, and the information obtained by the airborne camera 9 is transmitted to the flight control main controller 6 in the unmanned aerial vehicle 1;
s3, acquiring data information by using the sensor unit 10 in the flight process, and transmitting the acquired information to the flight control master controller 6 in the unmanned aerial vehicle 1;
s4, after the flight control master controller 6 acquires the information, the information is transmitted to the display control platform through the wireless communicator in time for information display, and meanwhile, the power supply battery 7 supplies power in time;
s5, acquiring position information through GPS module at moment when unmanned aerial vehicle 1 carries out airborne monitoring control in flight process
As a specific optimization scheme of this embodiment, the model of the flight control master controller 6 is KY12S, the GPS module is a GPS locator, and the model of the GPS locator is Air 800.
The invention has the beneficial effects that:
1. this unmanned aerial vehicle machine carries monitoring control device and control method, utilize machine-carried camera 9 to carry out information acquisition, utilize sensor unit 10 to carry out data information acquisition, will obtain information transmission for unmanned aerial vehicle 1 inside flight control master controller 6, in-process unmanned aerial vehicle 1 carries out machine-carried monitoring control the time and obtains positional information through the GPS module, can gather multiple information, information can in time collect the arrangement, fast carry out information display through showing control platform, reach better unmanned aerial vehicle machine-carried monitoring control's purpose.
2. This unmanned aerial vehicle machine carries monitoring control device and control method, at unmanned aerial vehicle 1's bottom through damping spring 82 cooperation backup pad 83 constitution damper, can carry out shock attenuation protection to unmanned aerial vehicle 1, simple structure does benefit to and prolongs its life.
3. According to the airborne monitoring control device and the control method of the unmanned aerial vehicle, the principle that the triangular arrangement is formed among the unmanned aerial vehicle 1, the tail frame 4 and the support frame 8 is beneficial to fully utilizing the stability of the triangle is formed, and therefore the unmanned aerial vehicle has good stability.
4. This unmanned aerial vehicle machine carries monitoring control device and control method can carry out the angle modulation to organism 93 and camera head 94 according to actual need, does benefit to and adjusts organism 93 and camera head 94 control snapshot angle, and then has improved the result of use.
Of course, the storage medium containing computer executable instructions provided by the embodiments of the present invention is not limited to the method operations described above, and may also perform related operations in the statistical method of user traffic of base target area mobile communication terminals provided by any embodiments of the present invention, and it is clear to those skilled in the art from the above description of the embodiments that the present invention can be implemented by software and necessary general hardware, and certainly, by hardware, but in many cases, the former is a better implementation, and based on such understanding, the technical solution of the present invention and the portions contributing to the prior art can be embodied in the form of software product, which can be stored in a computer readable storage medium, such as a floppy disk of a computer, A Read-Only Memory (ROM), a Random Access Memory (RAM), a FLASH Memory (FLASH), a hard disk or an optical disk, etc., which includes several instructions to make a computer device (which may be a personal computer, a server, or a network device, etc.) execute the method according to the embodiments of the present invention.
It should be noted that, in the embodiment of the above search apparatus, each included unit and module are merely divided according to functional logic, but are not limited to the above division as long as the corresponding functions can be implemented; in addition, specific names of the functional units are only for convenience of distinguishing from each other, and are not used for limiting the protection scope of the present invention.
It should be noted that the foregoing is only a preferred embodiment of the invention and the technical principles employed, and those skilled in the art will understand that the invention is not limited to the specific embodiments described herein, and that various obvious changes, rearrangements and substitutions can be made by those skilled in the art without departing from the scope of the invention. Therefore, although the present invention has been described in greater detail by the above embodiments, the present invention is not limited to the above embodiments, and may include other equivalent embodiments without departing from the spirit of the present invention, and the scope of the present invention is determined by the scope of the appended claims.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that 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 (10)
1. An airborne monitoring and controlling device of an unmanned aerial vehicle comprises the unmanned aerial vehicle (1), a driving motor (2), a propeller (3), a flight control main controller (6), a support frame (8) and an airborne camera (9), and is characterized in that the driving motor (2) is fixedly arranged at the top of the unmanned aerial vehicle (1), the propeller (3) is fixedly arranged on an output shaft of the driving motor (2), a tailstock (4) is fixedly arranged at the rear side of the unmanned aerial vehicle (1), the flight control main controller (6) and a power supply battery (7) are arranged at the bottom inside the unmanned aerial vehicle (1), the support frame (8) is arranged at the bottom of the unmanned aerial vehicle (1), the support frame (8) comprises a fixing seat (81), a damping spring (82) and a support plate (83), the support plate (83) is arranged at the bottom of the fixing frame (81), a sensor unit (10) is arranged at the top inside the unmanned aerial vehicle (1);
an airborne camera (9) is arranged on the front side of the bottom of the unmanned aerial vehicle (1), the airborne camera (9) comprises a fixed rod (91), a movable shaft (92), a machine body (93) and a camera head (94), the machine body (93) is movably arranged at the bottom of the fixed rod (91) through the movable shaft (92), and the camera head (94) is fixedly arranged at the bottom of the machine body (93);
the output electricity of airborne camera (9) and sensor unit (10) is connected with the input of unmanned aerial vehicle (1) inside flight control master controller (6), the output electricity of flight control master controller (6) is connected with driving motor (2) and wireless communicator's input, the two-way electricity of output of flight control master controller (6) is connected with the input of GPS module, the input electricity of flight control master controller (6) is connected with the input of remote controller.
2. The airborne monitoring and control device of the unmanned aerial vehicle as claimed in claim 1, wherein the output shaft of the driving motor (2) is fixedly provided with a rotating shaft, the surface of the rotating shaft is fixedly provided with a connecting rod, and one end of the connecting rod far away from the rotating shaft is provided with a propeller (3) through a fixed bolt connection.
3. The airborne monitoring and control device of unmanned aerial vehicle of claim 1, characterized in that the top of the tailstock (4) is fixedly provided with an auxiliary propeller (5), and the bottom of the auxiliary propeller (5) is provided with a motor.
4. The airborne monitoring and control device of the unmanned aerial vehicle of claim 1, characterized in that a fixing seat (81) is fixedly arranged at the bottom of the supporting frame (8), a damping spring (82) is fixedly arranged at the bottom of the fixing seat (81), and a supporting plate (83) is fixedly arranged at the bottom of the damping spring (82).
5. The airborne monitoring and control device of unmanned aerial vehicle of claim 1, characterized in that, the connection setting is carried out through the stiffener between tailstock (4) and support frame (8), constitute triangle-shaped setting between unmanned aerial vehicle (1), tailstock (4) and support frame (8).
6. The monitoring and control device on board an unmanned aerial vehicle of claim 1, wherein the body (93) and the camera head (94) are angularly adjustable between zero degrees and one hundred twenty degrees under the action of the movable shaft (92).
7. The airborne monitoring and control device of unmanned aerial vehicle of claim 1, characterized in that the output electricity of wireless communicator is connected with the input of display control platform, display device is provided with to the inside of display control platform.
8. The device of claim 1, wherein the sensor units comprise heavy metal detectors, smoke sensors, PM2.5 monitors, and PM10 monitors.
9. The method for monitoring and controlling the airborne condition of the unmanned aerial vehicle as claimed in any one of claims 1-8, comprising the steps of:
s1, sending an instruction to a flight control main controller (6) inside the unmanned aerial vehicle (1) by using a remote controller, controlling a driving motor (2) to work by using the flight control main controller (6), and driving a propeller (3) to rotate by using the rotation of the driving motor (2) so that the unmanned aerial vehicle (1) flies;
s2, in the flight process, an airborne camera (9) is used for collecting information, video and photo information is obtained, and the information obtained by the airborne camera (9) is transmitted to a flight control main controller (6) in the unmanned aerial vehicle (1);
s3, acquiring data information by using the sensor unit (10) in the flying process, and transmitting the acquired information to a flight control main controller (6) in the unmanned aerial vehicle (1);
s4, after the flight control master controller (6) acquires the information, the information is transmitted to the display control platform through the wireless communicator in time for information display, and meanwhile, the power supply battery (7) supplies power in time;
s5, acquiring the position information through the GPS module at all times when the unmanned aerial vehicle (1) carries out airborne monitoring control in the flight process.
10. The airborne monitoring control method of unmanned aerial vehicle of claim 9, characterized in that the model of said flight control master controller (6) is KY12S, said GPS module is a GPS locator, and said GPS locator is Air 800.
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