CN113247285A - Unmanned aerial vehicle and design method of three-dimensional air route of unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle and design method of three-dimensional air route of unmanned aerial vehicle Download PDFInfo
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- CN113247285A CN113247285A CN202110723587.9A CN202110723587A CN113247285A CN 113247285 A CN113247285 A CN 113247285A CN 202110723587 A CN202110723587 A CN 202110723587A CN 113247285 A CN113247285 A CN 113247285A
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- 238000000034 method Methods 0.000 title claims abstract description 14
- 230000035939 shock Effects 0.000 claims abstract description 23
- 239000006096 absorbing agent Substances 0.000 claims abstract description 13
- 230000007306 turnover Effects 0.000 claims description 8
- 238000010521 absorption reaction Methods 0.000 claims description 6
- 230000007547 defect Effects 0.000 claims description 6
- 210000000078 claw Anatomy 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims 1
- 238000013016 damping Methods 0.000 description 7
- 238000009434 installation Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000037237 body shape Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
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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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
- F16M11/12—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
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- Accessories Of Cameras (AREA)
Abstract
The invention provides an unmanned aerial vehicle and a three-dimensional air route design method of the unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The flight subassembly includes frame, support, unmanned aerial vehicle main part, driving motor and lifting fan, the adjusting part includes guide rail frame, trip shaft, first motor, roll-over table and second motor, the balance subassembly includes distribution platform, bumper shock absorber, shock attenuation platform, balanced seat, balancing stand, third motor and camera module. Vertical upset design breaks through current underlying shooting design, increases the shooting angle to the target, and the platform design is taken photograph to the double shot, improves the scope angle that unmanned aerial vehicle shot the photo, increases the overlap ratio of target body image, reduces unmanned aerial vehicle's flight orbit, and the horizontal rotation design, the shooting device breaks away from unmanned aerial vehicle self angular direction constraint, trails the target body in real time, reduces unmanned aerial vehicle course track, and unmanned aerial vehicle shooting angle is big, and unmanned aerial vehicle shoots and adjusts more conveniently.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a method for designing a three-dimensional air route of an unmanned aerial vehicle.
Background
The current unmanned plane route planning method comprises the following steps: according to the requirement of an unmanned aerial vehicle user, in a specified size range, an unmanned aerial vehicle air route is planned above a target in a broken line mode according to the flying height, the flying speed, the overlapping rate of shot photos and the predicted flying time. The cameras can respectively carry out orthographic shooting, shooting with the lens inclined forward by 45 degrees, shooting with the lens inclined backward by 45 degrees, shooting with the lens inclined leftward by 45 degrees, and shooting with the lens inclined rightward by 45 degrees. By switching the angle, the image information of the target area can be obtained.
But above-mentioned scheme still has certain defect, and the inventor finds through the research, is subject to the camera and puts the design down, needs often to adjust unmanned aerial vehicle's the angle of circling to adjust unmanned aerial vehicle shooting angle, and unmanned aerial vehicle can only shoot the target object by last to down, shoots the angle undersize and leads to image deformation, defect scheduling problem easily.
Disclosure of Invention
In order to make up for the defects, the invention provides a method for designing a three-dimensional air route of an unmanned aerial vehicle, and aims to solve the problem that the shooting angle of the unmanned aerial vehicle is limited.
The invention is realized by the following steps:
in a first aspect, the present invention provides a drone comprising a flight assembly, a conditioning assembly, and a balancing assembly.
The flight subassembly includes frame, support, unmanned aerial vehicle main part, driving motor and lift fan, support one end set up in frame week side, the unmanned aerial vehicle main part set up in on the support, the driving motor fuselage evenly sets up in keeping away from the frame support one end, the lift fan is fixed in the driving motor output, the adjusting part includes guide rail frame, trip shaft, first motor, roll-over table and second motor, the guide rail frame symmetry sets up in the frame, the trip shaft both ends rotate in between the guide rail frame, the first motor fuselage sets up in guide rail frame one side, the first motor output is fixed in trip shaft one end, the fixed cover of roll-over table lower extreme connect in the trip shaft surface, the second motor fuselage set up in on the roll-over table, the balanced subassembly includes the cloth table, The camera shooting device comprises a shock absorber, a shock absorption table, a balance seat, a balance frame, a third motor and a camera shooting module, wherein the distribution table is fixed at the output end of the second motor, the lower end of the shock absorber is uniformly arranged on the distribution table, the shock absorption table is arranged at the upper end of the shock absorber, the balance seat is symmetrically arranged on the shock absorption table, two ends of the balance frame are rotated between the upper ends of the balance seat, a body of the third motor is arranged at the upper end of the balance seat, the output end of the third motor is driven at the upper end of the balance frame, and the camera shooting module is arranged on the balance frame.
In one embodiment of the invention, one side of the lower end of the support is rotatably provided with an undercarriage, the other side of the lower end of the support is rotatably provided with a hydraulic cylinder, and a cylinder body of the hydraulic cylinder rotates at the lower end of the undercarriage, so that the hydraulic cylinder is suitable for rising and falling of various inclined planes of the unmanned aerial vehicle and simultaneously reduces impact vibration during landing through hydraulic damping.
In one embodiment of the invention, the clamp claws are symmetrically arranged on one side of the guide rail frame and clamped on the surface of the frame, so that the shooting device and the unmanned aerial vehicle can be conveniently and rapidly installed and positioned, and meanwhile, the shooting device is supported to avoid the unmanned aerial vehicle.
In an embodiment of the invention, an installation table is arranged on one side of the guide rail frame, and the first motor body is fixed on the installation table, so that the first motor is convenient to install and position.
In one embodiment of the invention, the bottom of the overturning platform is provided with a block, the bottom of the block is provided with a clamping seat, and the clamping seat is fixedly sleeved on the surface of the overturning shaft, so that the shooting device is fixedly overturned, and meanwhile, the unmanned aerial vehicle is supported and avoided.
In one embodiment of the invention, the support plates are uniformly arranged on the surface of the distribution table, and the lower ends of the shock absorbers are arranged on the support plates, so that the shock absorption area of the shock absorbers is increased, and the extension of the installation platform of the shooting device is facilitated.
In an embodiment of the invention, a swivel base is arranged at the upper end of the balance seat far away from the third motor, a balance shaft is arranged at the upper end of the balance frame far away from the third motor, and one end of the balance shaft rotates in the swivel base.
In an embodiment of the invention, a supporting seat is arranged on one side of the balance frame, a connecting seat is arranged at the bottom of the camera module, and the lower end of the connecting seat rotates to the supporting seat, so that the angle of the shooting device is further adjusted.
In one embodiment of the invention, the upper end of the supporting seat is provided with a locking bolt and a locking nut, one end of the locking bolt penetrates through the connecting seat, the locking nut is in threaded connection with the surface of the locking bolt, and one side of the locking nut is attached to the upper end of the supporting seat, so that the shooting device can be conveniently and rapidly mounted.
In a second aspect, the present invention further provides a method for designing a three-dimensional route of an unmanned aerial vehicle, which uses the unmanned aerial vehicle, including the following steps:
the second motor is used for realizing horizontal 360-degree shooting of the double camera modules, so that the double camera modules are separated from the angle direction constraint of the unmanned aerial vehicle, the shape of a target body is tracked in real time, the route track of the unmanned aerial vehicle is reduced, and the shooting and flying efficiency of the unmanned aerial vehicle is improved;
the first motor and the third motor are used for realizing vertical 180-degree shooting of the double camera modules, the first motor drives the machine body of the double camera modules to break through the original limitation that the double camera modules only shoot above a target area, and the third motor adjusts the focusing angle of the double camera modules to solve the problems of image deformation, defects and the like caused by small-angle shooting in the original vertical direction;
through first motor, second motor and the two camera module of third motor common control shooting angle, improve the scope that unmanned aerial vehicle shot the photo, increase the overlap ratio of target body image, reduce unmanned aerial vehicle's flight orbit, improve unmanned aerial vehicle and shoot and flight efficiency.
The invention has the beneficial effects that: the invention obtains a design method of a three-dimensional air route of an unmanned aerial vehicle through the design, when in use, the shooting device is symmetrically clamped into a rack to be locked and fixed through a guide rail frame, a double-shooting platform keeps the unmanned aerial vehicle balanced, a first motor is turned on to drive the shooting device to rotate 180 degrees in the vertical direction, the original limitation that the shooting is only carried out above a target area is broken through, the off-plane height of the shooting device is expanded through a turnover table to reduce the shooting obstacle limitation, a second motor is turned on to control the shooting device to rotate 360 degrees in the horizontal direction, a target object is tracked through shooting angle control, the unmanned aerial vehicle rotates spirally and rotates in a self-rotation mode, a shock absorber is used to reduce the flying shock in the shooting process of the unmanned aerial vehicle, a third motor is used to control the shooting device to rotate vertically in a small range to match with the first motor to, the increase is to the shooting angle of target object, adopts the design of the platform of taking a picture of two shots, improves the scope angle that unmanned aerial vehicle shot the photo, increases the overlap ratio of target body image, reduces unmanned aerial vehicle's flight track, adopts the horizontal rotation design, and the shooting device breaks away from unmanned aerial vehicle self angular direction constraint, trails the target body shape in real time, reduces unmanned aerial vehicle course line orbit, and unmanned aerial vehicle shoots the angle big, and unmanned aerial vehicle shoots and adjusts more conveniently.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle according to an embodiment of the present invention;
FIG. 2 is a schematic perspective view of a flight assembly according to an embodiment of the present invention;
FIG. 3 is a schematic perspective view of an adjustment assembly according to an embodiment of the present invention;
FIG. 4 is a schematic perspective view of a first perspective view of a balancing assembly according to an embodiment of the present invention;
FIG. 5 is a perspective view of a second perspective view of a balancing assembly according to an embodiment of the present invention;
fig. 6 is a schematic structural diagram of an unmanned aerial vehicle according to an embodiment of the present invention.
In the figure: 100-a flight assembly; 110-a rack; 120-a scaffold; 121-a landing gear; 122-a hydraulic cylinder; 130-a drone main body; 140-a drive motor; 150-lifting fan; 300-an adjustment assembly; 310-a rail mount; 311-a jaw; 312-a mounting table; 320-a turning shaft; 330-a first motor; 340-a turning table; 341-block of bed hedgehopping; 342-a card seat; 350-a second motor; 500-a balancing assembly; 510-a distribution table; 511-brace; 520-a shock absorber; 530-a damping table; 540-balance seat; 541-transposition; 550-a balancing stand; 551-balance shaft; 552-a support base; 553-a locking bolt; 554-a locking nut; 560-a third motor; 570-camera module; 571-connecting seat.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings of the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.
Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the equipment or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be considered as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
Referring to fig. 1, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle includes flight assembly 100, adjusting part 300 and balanced subassembly 500, adjusting part 300 is installed on flight assembly 100, balanced subassembly 500 is installed on adjusting part 300, flight assembly 100 carries the flight of shooting device, and carry out whole profile around the flight around the target object, adjusting part 300 breaks through current camera device and puts the design down, through the rotatory shooting angle that increases of vertical direction and horizontal direction, balanced subassembly 500 reduces the vibrations of flight in-process, and through small-amplitude angle modulation, adjust the focus of making a video recording.
Referring to fig. 1 and 2, the flying assembly 100 includes a frame 110, a bracket 120, an unmanned aerial vehicle main body 130, a driving motor 140 and a lifting fan 150, one end of the bracket 120 is disposed on the periphery of the frame 110, the bracket 120 is bolted to the frame 110, the unmanned aerial vehicle main body 130 is disposed on the bracket 120, the unmanned aerial vehicle main body 130 is bolted to the bracket 120, the body of the driving motor 140 is uniformly disposed on one end of the bracket 120 away from the frame 110, the driving motor 140 is bolted to the bracket 120, the lifting fan 150 is fixed to the output end of the driving motor 140, the lifting fan 150 is in threaded connection with the driving motor 140, a landing gear 121 is rotatably disposed on one side of the lower end of the bracket 120, a hydraulic cylinder 122 is rotatably disposed on the other side of the lower end of the bracket 120, the cylinder body of the hydraulic cylinder 122 rotates on the lower end of the landing gear 121, the specific landing gear 121 is respectively rotatably connected to the bracket 120 and the pin of the hydraulic cylinder 122, and the hydraulic cylinder 122 controls the supporting angle of the landing gear 121, impact vibration when landing is reduced through hydraulic shock attenuation when the various unmanned aerial vehicle inclined plane of adaptation rises and falls.
Referring to fig. 1 and 3, the adjusting assembly 300 includes a guide rail frame 310, a turning shaft 320, a first motor 330, a turning table 340 and a second motor 350, the guide rail frame 310 is symmetrically disposed on the frame 110, a jaw 311 is symmetrically disposed on one side of the guide rail frame 310, the jaw 311 is integrally formed with the guide rail frame 310, the jaw 311 is fastened to the surface of the frame 110, in a specific embodiment, a boss is disposed on the surface of the frame 110, the jaw 311 is quickly positioned on the boss through a bottom groove and then fixed by a bolt, two ends of the turning shaft 320 rotate between the guide rail frames 310, in this embodiment, the surface of the turning shaft 320 is attached to an inner arc track of the guide rail frame 310 to realize stable rotation of the turning shaft 320, a body of the first motor 330 is disposed on one side of the guide rail frame 310, a mounting table 312 is disposed on one side of the guide rail frame 310, the mounting table 312 is integrally formed with the guide rail frame 310, the body of the first motor 330 is fixed on the mounting table 312, and the first motor 330 is connected with the mounting table 312 by a bolt, the particular first motor 330 controls the rotation angle of the tumble shaft 320.
Wherein, the output end of the first motor 330 is fixed on one end of the turning shaft 320, the first motor 330 is connected with the turning shaft 320 by a bolt, the lower end of the turning table 340 is fixedly sleeved on the surface of the turning shaft 320, the bottom of the turning table 340 is provided with a block 341 which is raised, the turning table 340 is connected with the block 341 which is raised by a bolt, in the concrete embodiment, the block 341 which is raised increases the supporting height of the turning table 340 to facilitate the avoidance of the shooting device and the unmanned aerial vehicle in the rotation process, the bottom of the block 341 which is raised is provided with a clamping seat 342 which is connected with the clamping seat 341 by a bolt, the clamping seat 342 is fixedly sleeved on the surface of the turning shaft 320, in the concrete embodiment, the clamping seat 342 is sleeved on the surface of the turning shaft 320 by two semicircular structures and is fixedly locked by a bolt to realize the rotation fixation of the shooting device, compared with the traditional rotation structure, the structure can break through the limit of the unmanned aerial vehicle body, realize the up-down and-up movement of the space of the shooting device, and the support sliding of the double-arc track, the supporting strength of the shooting device is improved, the body of the second motor 350 is arranged on the overturning platform 340, the second motor 350 is connected with the overturning platform 340 through bolts, and the second motor 350 drives the shooting device to rotate horizontally by 360 degrees, so that the shooting angle is further increased.
Referring to fig. 1, 4 and 5, the balance assembly 500 includes a distribution table 510, a damper 520, a damping table 530, a balance seat 540, a balance frame 550, a third motor 560 and a camera module 570, the distribution table 510 is fixed at an output end of the second motor 350, the distribution table 510 is connected with the second motor 350 by bolts, the distribution table 510 specifically extends a range of a support platform of the camera device to facilitate angle adjustment of the camera device, a lower end of the damper 520 is uniformly disposed on the distribution table 510, the damping table 530 is disposed at an upper end of the damper 520, a support plate 511 is uniformly disposed on a surface of the distribution table 510, a lower end of the damper 520 is disposed on the support plate 511 to reduce a weight of the distribution table 510 and increase a support area, the damper 520 is respectively connected with the support plate 511 and the damping table 530 by threads, thereby reducing shaking of the camera device caused by an air flow during a flight, improving a shooting stability, the balance seat 540 is symmetrically disposed on the damping table 530, the balance base 540 is connected with the damping table 530 through bolts, and both ends of the balance frame 550 are rotated between the upper ends of the balance base 540.
Wherein, the body of the third motor 560 is arranged at the upper end of the balance seat 540, the third motor 560 is connected with the balance seat 540 by bolts, the output end of the third motor 560 is transmitted at the upper end of the balance frame 550, the third motor 560 is connected with the balance frame 550 by bolts, the third motor 560 controls the balance frame 550 to rotate in a small way, and the shooting focus is adjusted in a matching way, so that the body of the shooting device which rotates vertically can be adjusted again, the upper end of the balance seat 540 far away from the third motor 560 is provided with a swivel 541, the swivel 541 is connected with the balance seat 540 by bolts, the upper end of the balance frame 550 far away from the third motor 560 is provided with a balance shaft 551, the balance shaft 551 is connected with the balance frame 550 by bolts, one end of the balance shaft 551 rotates in the swivel 541, the camera module 570 is arranged on the balance frame 550, one side of the balance frame 550 is provided with a supporting seat 552 which is connected with the balance frame 550 by bolts, the bottom of the camera module 570 is provided with a connecting seat 571 by bolts, the camera module 570 and the connecting seat 571 is connected with the connecting seat, the lower end of the connecting seat 571 is rotated on the supporting seat 552, the connecting seat 571 is connected with the supporting seat 552 through a pin shaft, and the installation angle of the camera device can be adjusted conveniently through the supporting seat 552.
The upper end of the supporting seat 552 is provided with a locking bolt 553 and a locking nut 554, one end of the locking bolt 553 penetrates through the connecting seat 571, the locking nut 554 is screwed on the surface of the locking bolt 553, one side of the locking nut 554 is attached to the upper end of the supporting seat 552, and the connecting seat 571 and the supporting seat 552 are fixed through the structure.
The invention also provides a method for designing the three-dimensional air route of the unmanned aerial vehicle, which utilizes the unmanned aerial vehicle and comprises the following steps:
the second motor 350 is used for realizing horizontal 360-degree shooting of the double camera modules 570, so that the double camera modules 570 are separated from the angle direction constraint of the unmanned aerial vehicle, the shape of a target body is tracked in real time, the route track of the unmanned aerial vehicle is reduced, and the shooting and flying efficiency of the unmanned aerial vehicle is improved;
the first motor 330 and the third motor 560 are used for realizing vertical 180-degree shooting of the double camera modules 570, the first motor 330 drives the bodies of the double camera modules 570 to break through the original limitation that the double camera modules 570 are only shot above a target area, and the third motor 560 is used for adjusting the focusing angles of the double camera modules 570 so as to make up the problems of image deformation, defects and the like caused by small-angle shooting in the original vertical direction;
through first motor 330, second motor 350 and third motor 560 common control two camera module 570 shooting angles, improve the scope that unmanned aerial vehicle shot the photo, increase the overlapping rate of target body image, reduce unmanned aerial vehicle's flight orbit, improve unmanned aerial vehicle and shoot and flight efficiency.
Specifically, this unmanned aerial vehicle theory of operation: when the unmanned aerial vehicle is used, the shooting devices are quickly and symmetrically clamped into the rack 110 through the guide rail frame 310 to be locked and fixed, the double-shooting platform keeps the unmanned aerial vehicle balanced, the first motor 330 is started to drive the shooting devices to rotate for 180 degrees in the vertical direction, the original limitation that the shooting is only carried out above a target area is broken through, the off-plane height of the shooting devices is expanded through the overturning platform 340, the shooting obstacle limitation is reduced, the second motor 350 is started to control the shooting devices to rotate for 360 degrees in the horizontal direction, the target object is tracked through shooting angle control, the spiral rotation of the unmanned aerial vehicle is reduced, the flying vibration in the shooting process of the unmanned aerial vehicle is reduced through the shock absorber 520, the shooting devices are controlled to rotate vertically for a small extent through the third motor 560, the shooting angle adjustment is carried out on the target object by matching with the first motor 330, the shooting devices can freely move up and down, the existing space constraint is broken through, the shooting angle of the target object is increased, and the double-platform shooting platform balances the unmanned aerial vehicle in flight balance, carry out the shooting of bigger regional angle to the target in the unit space, the horizontal rotation that the shooting device can be free need not to adjust unmanned aerial vehicle flight angle, tracks through shooting device self angle modulation, and the real-time tracking target shape, unmanned aerial vehicle course track is shorter, and unmanned aerial vehicle shoots the angle big, and unmanned aerial vehicle shoots and adjusts more conveniently.
It should be noted that the specific model specifications of the main body 130, the driving motor 140, the first motor 330, the second motor 350, the third motor 560 and the camera module 570 of the unmanned aerial vehicle need to be determined by type selection according to the actual specification of the device, and the specific type selection calculation method adopts the prior art in the field, and therefore details are not repeated.
The power supply and the principle of the main body 130 of the drone, the driving motor 140, the first motor 330, the second motor 350, the third motor 560 and the camera module 570 are clear to those skilled in the art and will not be described in detail here.
The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention, and various modifications and changes may be made to the present invention by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle, comprising:
the flight assembly (100) comprises a rack (110), a support (120), an unmanned aerial vehicle main body (130), a driving motor (140) and a lifting fan (150), wherein one end of the support (120) is arranged on the peripheral side of the rack (110), the unmanned aerial vehicle main body (130) is arranged on the support (120), the body of the driving motor (140) is uniformly arranged on one end of the support (120) far away from the rack (110), and the lifting fan (150) is fixed at the output end of the driving motor (140);
the adjusting assembly (300) comprises a guide rail frame (310), a turnover shaft (320), a first motor (330), a turnover table (340) and a second motor (350), wherein the guide rail frame (310) is symmetrically arranged on the rack (110), two ends of the turnover shaft (320) are rotated between the guide rail frame (310), a machine body of the first motor (330) is arranged on one side of the guide rail frame (310), an output end of the first motor (330) is fixed at one end of the turnover shaft (320), the lower end of the turnover table (340) is fixedly sleeved on the surface of the turnover shaft (320), and a machine body of the second motor (350) is arranged on the turnover table (340);
a balancing assembly (500), the balancing assembly (500) comprising a distribution table (510), a shock absorber (520), a shock absorbing table (530), a balancing stand (540), a balancing stand (550), a third motor (560) and a camera module (570), the distribution table (510) is fixed at the output end of the second motor (350), the lower ends of the shock absorbers (520) are uniformly arranged on the distribution table (510), the shock absorption table (530) is arranged at the upper end of the shock absorber (520), the balance seats (540) are symmetrically arranged on the shock absorption table (530), the two ends of the balancing stand (550) rotate between the upper ends of the balancing seats (540), the body of the third motor (560) is arranged at the upper end of the balance seat (540), the output end of the third motor (560) is transmitted to the upper end of the balancing stand (550), and the camera module (570) is arranged on the balancing stand (550).
2. An unmanned aerial vehicle according to claim 1, wherein the lower end of the support (120) is rotatably provided with a landing gear (121) on one side, and the lower end of the support (120) is rotatably provided with a hydraulic cylinder (122) on the other side, and the cylinder body of the hydraulic cylinder (122) is rotated on the lower end of the landing gear (121).
3. The unmanned aerial vehicle of claim 1, wherein the guide rail frame (310) is symmetrically provided with claws (311) at one side, and the claws (311) are clamped on the surface of the frame (110).
4. An unmanned aerial vehicle according to claim 1, wherein the guide rail frame (310) is provided with a mounting table (312) on one side, and the first motor (330) body is fixed on the mounting table (312).
5. The unmanned aerial vehicle of claim 1, wherein the flipping table (340) is provided with a block (341) at the bottom, the block (341) is provided with a cassette (342) at the bottom, and the cassette (342) is fixedly sleeved on the surface of the flipping shaft (320).
6. An unmanned aerial vehicle according to claim 1, wherein the distribution table (510) is provided with a support plate (511) uniformly on the surface, and the lower ends of the shock absorbers (520) are arranged on the support plate (511).
7. An unmanned aerial vehicle according to claim 1, wherein a swivel base (541) is arranged at the upper end of the balancing base (540) far away from the third motor (560), a balancing shaft (551) is arranged at the upper end of the balancing frame (550) far away from the third motor (560), and one end of the balancing shaft (551) rotates in the swivel base (541).
8. The unmanned aerial vehicle of claim 1, wherein a supporting seat (552) is disposed on one side of the balancing stand (550), a connecting seat (571) is disposed at the bottom of the camera module (570), and the lower end of the connecting seat (571) rotates on the supporting seat (552).
9. The unmanned aerial vehicle of claim 8, wherein a locking bolt (553) and a locking nut (554) are arranged at the upper end of the supporting seat (552), one end of the locking bolt (553) penetrates through the connecting seat (571), the locking nut (554) is screwed on the surface of the locking bolt (553), and one side of the locking nut (554) is attached to the upper end of the supporting seat (552).
10. An unmanned aerial vehicle three-dimensional route design method which utilizes the unmanned aerial vehicle of any one of claims 1-9, characterized by comprising the following steps:
horizontal 360-degree shooting of the double camera modules (570) is achieved through the second motor (350), the double camera modules (570) are separated from the self angle direction constraint of the unmanned aerial vehicle, the shape of a target body is tracked in real time, and the route track of the unmanned aerial vehicle is reduced;
the vertical 180-degree shooting of the double camera modules (570) is realized through the first motor (330) and the third motor (560), the first motor (330) drives the bodies of the double camera modules (570) to break through the original limitation that the double camera modules (570) only shoot above a target area, and the third motor (560) adjusts the focusing angles of the double camera modules (570) to make up the problems of image deformation and defects caused by small-angle shooting in the original vertical direction;
through first motor (330), second motor (350) and third motor (560) common control two camera module (570) shooting angle, improve the scope that unmanned aerial vehicle shot the photo, increase the overlap ratio of target body image, reduce unmanned aerial vehicle's flight path.
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113606466A (en) * | 2021-10-08 | 2021-11-05 | 成都理工大学 | Portable binocular photogrammetry device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114882A (en) * | 2016-08-25 | 2016-11-16 | 四川马可视觉网络科技有限公司 | No-manned plane three-dimensional rotating camera erecting device |
| CN206826921U (en) * | 2017-03-21 | 2018-01-02 | 西南科技大学 | A kind of mobile platform based on rotor |
| US20190118969A1 (en) * | 2015-11-06 | 2019-04-25 | Spherie Ug | Wingless aircraft |
| CN110001945A (en) * | 2019-04-16 | 2019-07-12 | 中国电建集团西北勘测设计研究院有限公司 | One kind facade that falls precipice finely tilts boat and takes the photograph device and method for imaging |
| CN209454997U (en) * | 2018-12-18 | 2019-10-01 | 乔燕英 | Unmanned plane for aerophotogrammetry |
| CN111846267A (en) * | 2020-08-06 | 2020-10-30 | 成都市玄上科技有限公司 | Shooting method and device for oblique photography three-dimensional modeling |
-
2021
- 2021-06-29 CN CN202110723587.9A patent/CN113247285A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20190118969A1 (en) * | 2015-11-06 | 2019-04-25 | Spherie Ug | Wingless aircraft |
| CN106114882A (en) * | 2016-08-25 | 2016-11-16 | 四川马可视觉网络科技有限公司 | No-manned plane three-dimensional rotating camera erecting device |
| CN206826921U (en) * | 2017-03-21 | 2018-01-02 | 西南科技大学 | A kind of mobile platform based on rotor |
| CN209454997U (en) * | 2018-12-18 | 2019-10-01 | 乔燕英 | Unmanned plane for aerophotogrammetry |
| CN110001945A (en) * | 2019-04-16 | 2019-07-12 | 中国电建集团西北勘测设计研究院有限公司 | One kind facade that falls precipice finely tilts boat and takes the photograph device and method for imaging |
| CN111846267A (en) * | 2020-08-06 | 2020-10-30 | 成都市玄上科技有限公司 | Shooting method and device for oblique photography three-dimensional modeling |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113606466A (en) * | 2021-10-08 | 2021-11-05 | 成都理工大学 | Portable binocular photogrammetry device |
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Application publication date: 20210813 |