Unmanned aerial vehicle control device and method

Abstract

The invention provides an unmanned aerial vehicle control device which comprises six groups of power rotary blades and a lower supporting seat, and the six groups of power rotary blades are uniformly distributed on the outer side of a main body in an annular structure. Compared with the prior art, the unmanned aerial vehicle control device has the following beneficial effects that a supporting ring seat is used for providing a supporting effect with an inner supporting frame; the lower end of the supporting ring seat is supported by using the adjusting bracket, the height of the signal receiving and transmitting module is adjusted by using the electric telescopic rod, and the interior of the main machine body is protected by using the waterproof shell; the invention also provides a control method of the unmanned aerial vehicle control device, which comprises the following steps that: firstly, a worker transmits an operation control instruction by using the remote controller, and after the signal receiver receives the operation control instruction transmitted by the remote controller, the control instruction is compiled through the controller; and power control is carried out on the flat motor and the side motor according to an operation control instruction transmitted by the remote controller.

Description

Technical Field

[0001] The present invention relates to a drone control device and method, belonging to the technical field of drones. Background Art

[0002] The control system of a drone consists of three main parts: flight control, navigation, and communication. The flight control system is responsible for the stability and control of the drone, the navigation system ensures that the drone flies along the predetermined route, and the communication system allows the operator to remotely control the drone or receive data transmitted by the drone. With the development of artificial intelligence technology, more and more drones have begun to have the ability to fly autonomously and can perform complex tasks without human intervention. If a drone cannot quickly collect multiple key data during flight, it may cause a series of problems, affecting the performance, safety, and mission execution capabilities of the drone.

[0003] Delays or failures in data collection can affect the navigation and control of drones, which rely on real-time data to adjust their flight paths and attitudes, such as GPS signals, accelerometers, gyroscopes, and magnetometers. If these data cannot be collected quickly, the drone may deviate from its intended route, leading to mission failure or even a collision or crash. Therefore, a drone control device and method are urgently needed to solve the above problems. Summary of the invention

[0004] In view of the deficiencies in the prior art, the purpose of the present invention is to provide a drone control device and method, which solves the problems raised in the above-mentioned background technology by adding power rotor blades and flat motors.

[0005] The technical solution of the present invention is implemented as follows: a drone control device comprises: power rotor blades and a lower support seat, wherein the power rotor blades are provided in six groups, and the six groups of power rotor blades are in an annular structure and are evenly distributed on the outside of the main body;

[0006] A group of flat motors for providing power to the power rotors are provided at the lower end of each group of power rotors, a group of inner support frames for limiting and connecting the outer sides of the flat motors are provided on the outer sides of the flat motors, and a group of support ring seats for providing support effects with the inner support frames are provided on the outer sides of the inner support frames;

[0007] The support ring seat is a hollow structure, and a group of air cavities for circulating air upward are provided inside the support ring seat. The cross-section of the support ring seat when viewed from above is a circular structure. A group of adjustment brackets for supporting the lower end of the support ring seat are provided on the right side of the support ring seat. The support ring seat can provide a supporting effect together with the internal support bracket, and the lower end of the support ring seat can be supported by using the adjustment brackets.

[0008] As a preferred embodiment, a group of adjustment components for adjusting the height of the adjustment bracket and the power rotor blades are provided on the inner side of the right side of the adjustment bracket, and a main body is provided on the inner side of several groups of the adjustment components;

[0009] The upper end of the main body is provided with a group of signal transceiver modules for performing signal transceiver functions, the signal transceiver modules and the main body are in an integrated structure, and the lower end of the signal transceiver modules is provided with a group of electric telescopic rods for adjusting the height thereof, and the lower end of the main body is provided with a group of lower support seats for slowly releasing the lower end of the main body;

[0010] The lower support seat is a movable mechanism, the main body has a circular cross-section when viewed from above, a group of waterproof shells for protecting the interior of the main body are provided on the outside of the main body, and a group of rubber sealing rings are provided at the connection between the waterproof shell and the main body. The height of the signal transceiver module can be adjusted by using an electric telescopic rod, the interior of the main body can be protected by using a waterproof shell, and water can be prevented from penetrating into the interior of the main body by using rubber sealing rings.

[0011] As a preferred embodiment, a group of control combination sensing modules for controlling signal reception and transmission are provided inside the main body, and the control combination sensing module includes a speed sensing module, a power control module, a picture acquisition module, a satellite positioning module, a level detection module, a height sensing module and a controller, and the speed sensing module, the power control module, the picture acquisition module, the satellite positioning module, the level detection module and the height sensing module are all connected to the controller through wires.

[0012] As a preferred embodiment, the adjustment assembly includes an inner movable shaft and an insert seat, and the left side of the inner movable shaft and the right side of the adjustment bracket are mutually sleeved, connected and fixed;

[0013] A group of small servo motors are arranged on the outer side of the inner movable shaft for driving the inner movable shaft to rotate actively, and the driving end of the small servo motor is connected to the inner movable shaft by power, and a group of lower support platforms are arranged on the upper end of the inner movable shaft for providing support effect to the inner movable shaft, and the cross section of the lower support platform is arranged in an L-shaped structure;

[0014] The lower support platform is made of a metal material, and a group of connecting dowels are provided at the upper end of the lower support platform for providing a connecting and supporting effect for the lower support platform. The connecting dowels and the lower support platform are an integral forging structure, and the lower support platform and the embedding seat are embedded and connected with each other. The cross-section of the embedding seat is a concave structure, and the embedding seat and the lower support platform are movably connected through a group of shafts. The embedding seat and the main body are an integral structure, and can provide a supporting effect for the inner movable shaft by using the lower support platform, and can provide a connecting and supporting effect for the lower support platform by using the lower connecting dowels.

[0015] As a preferred embodiment, the side acquisition component includes a camera embedded shell and a lower movable embedded seat, the right side cross section of the camera embedded shell is a ring structure, and a group of camera bodies for capturing images at the lower end of the main body are arranged inside the camera embedded shell;

[0016] A group of horizontal rotating seats for horizontally rotating the camera embedded shell is provided at the lower end of the camera embedded shell, a group of mounting frames for supporting the horizontal rotating seats are provided at the lower end of the horizontal rotating seats, a group of axial rotating columns for driving the camera embedded shell to flip up and down are provided on the front side of the mounting frames, a group of side motors for flipping the camera embedded shell to the left and right positions are provided on the front side of the axial rotating columns, and a group of outer embedded shells for limiting the movement of the side motors are provided on the outer side of the side motors;

[0017] The cross-section of the outer embedded shell is an inverted U-shaped structure, and the lower end of the outer embedded shell is provided with a group of lower support frames for supporting it, and the lower support frame and the outer embedded shell are fixed by two groups of bolts, and the lower end of the right side of the lower support frame is provided with a group of lower movable seats for movably engaging with the main body, and the right side of the lower support frame is provided with a group of inner teeth for maintaining directional movement thereof, and the right side of the inner teeth is provided with a group of adjusting gears for actively adjusting the forward and backward movement of the lower support frame, and the adjusting gears are meshed with the inner teeth, so that the outer embedded shell can be supported by using the lower support frame, can be movably engaged with the main body by using the lower movable seat, can maintain directional movement of the lower support frame by using the inner teeth, and can actively adjust the forward and backward movement of the lower support frame by using the adjusting gears.

[0018] As a preferred embodiment, the lower support seat includes a lower heat dissipation support and a lower sealing ring, the cross section of the lower support seat in a top view is a circular structure, the lower support seat is a movable structure, and the upper end of the lower support seat is connected to the lower end of the main body through a plurality of groups of air damping rods;

[0019] A group of semiconductor refrigeration sheets for actively cooling the interior of the main body are provided at the middle position of the lower end of the main body, the upper end of the semiconductor refrigeration sheet is a cooling end, the lower end of the semiconductor refrigeration sheet is a heat dissipation end, and a group of embedded grooves for limiting the installation of the semiconductor refrigeration sheet are provided on the outer side of the semiconductor refrigeration sheet;

[0020] A group of lower heat sinks for conducting heat to the heat dissipation end of the semiconductor refrigeration plate are arranged on the outside of the embedded groove. The cross-section of the lower heat sink is a ring structure when viewed from above. The lower heat sink is made of an aluminum alloy material. Several groups of heat sinks for ventilating the heat dissipation end of the semiconductor refrigeration plate are dispersed inside the lower heat sink. The semiconductor refrigeration plate can be used to actively cool the inside of the main body, the lower heat sink can be used to conduct heat to the heat dissipation end of the semiconductor refrigeration plate, and the heat sink can be used to ventilate the heat dissipation end of the semiconductor refrigeration plate.

[0021] As a preferred embodiment, the heat dissipation grooves of the plurality of groups are distributed in an annular structure, the interiors of the heat dissipation grooves of the plurality of groups are interconnected with the interiors of the embedded grooves, and the lower end of the lower heat dissipation support is provided with four groups of support feet for positioning and installing the lower heat dissipation support;

[0022] A group of inner spring seat rods for pressing and fitting the outer sides of each group of support legs are provided inside, a group of self-tapping screw heads for screwing with the inner force guide rods are provided at the lower ends of the inner spring seat rods, and a group of inner compression rods for providing elastic tension potential energy are provided inside the inner spring seat rods;

[0023] The inner compression rod is a pneumatic damping rod, and a group of bases for supporting its bottom are provided at the lower end of the inner compression rod, and a group of lower embedded sealing rings for sealing and engaging with the lower embedded seat are provided at the lower end of the base. The inner compression rod can provide elastic tension potential energy by using the inner compression rod, and can be screwed with the inner guide rod thread by using a self-tapping screw head.

[0024] As a preferred embodiment, the lower support seat further comprises an upper guide seat and a neutral rod, the cross section of the upper guide seat in a top view is a ring structure, and a group of external support rods for supporting the lower end of the upper guide seat are provided at the lower ends of the left and right sides;

[0025] A group of stress-bearing rods for bearing the pressure of the lower end of the lower embedded seat are provided at both left and right ends of the inner side of the upper guide seat, the lower ends of the two groups of stress-bearing rods are movably connected by shafts, and a group of neutral rods for transmitting the pressure borne by the two groups of stress-bearing rods are provided inside the lower ends of the two groups of stress-bearing rods;

[0026] The lower end of the neutral rod is provided with a group of lower supporting beams for bearing pressure on the lower end thereof, and the left and right sides of the lower supporting beams are connected and fixed with the two groups of outer supporting rods, and the lower ends of the middle positions of the two groups of stress-bearing rods are provided with a group of internal pressure holding springs for bearing pressure thereon, and the left and right ends of the inner sides of the internal pressure holding springs are provided with a group of internal movable grooves 1 and 2 for guiding the moving positions of the two groups of stress-bearing rods;

[0027] The inner movable groove 1 and the inner movable groove 2 have the same specifications, and the inner movable groove 1 is arranged on the left side, and the inner movable groove 2 is arranged on the right side. The lower end of the inner pressure holding spring is provided with a group of supporting beams for supporting its lower end. The supporting beam is a fixed structure and is connected and fixed to the lower end of the inner pressure holding spring. It can bear pressure on the lower end of the neutral rod by using the lower supporting beam, and can bear pressure on the two groups of force-bearing pressure rods by using the inner pressure holding spring.

[0028] A method for controlling an unmanned aerial vehicle comprises the following steps: first, a staff member transmits an operation control instruction by using a remote controller, and after a signal receiver receives the operation control instruction transmitted by the remote controller, the staff member compiles the control instruction by using the controller, and performs power control on a flat motor and a side motor according to the operation control instruction transmitted by the remote controller, thereby controlling the unmanned aerial vehicle; at the same time, a speed sensing module, a power control module, a picture acquisition module, a satellite positioning module, a level detection module, and a height sensing module inside the main body of the unmanned aerial vehicle can convert a digital signal into an analog signal through a digital-to-analog converter integrated inside the controller, and transmits the numerical information detected by each module to the remote controller end through a signal transceiver module, and displays it through a digital display screen; after a signal receiver receives the operation control instruction transmitted by the remote controller by using the controller, the staff member compiles the control instruction by using the controller, and performs power control on a flat motor and a side motor according to the operation control instruction transmitted by the remote controller; the speed sensing module, the power control module, the picture acquisition module, the satellite positioning module, the level detection module, and the height sensing module can be used to transmit the numerical information detected by each module to the remote controller end through a signal transceiver module, and display it through a digital display screen.

[0029] After adopting the above technical solution, the beneficial effects of the device are: by using the support ring seat to provide a supporting effect with the internal support frame, by using the adjustment support frame to support the lower end of the support ring seat, by using the electric telescopic rod to adjust the height of the signal transceiver module, and by using the waterproof shell to protect the inside of the main body;

[0030] The rubber sealing ring is used to prevent water from penetrating into the main body, the lower support seat is used to provide support for the inner movable shaft, the lower connecting tail is used to provide a connection support effect for the lower support seat, the lower support frame is used to carry the outer embedded shell, the lower movable embedded seat is used to movably engage with the main body, and the inner embedded teeth are used to keep the lower support frame directional movement;

[0031] The lower support frame can be actively adjusted to move forward and backward by using the adjusting gear, the inside of the main body can be actively cooled by using the semiconductor cooling sheet, and the heat dissipation end of the semiconductor cooling sheet can be heat-conducted by using the lower heat dissipation support;

[0032] By using heat dissipation grooves to ventilate the area around the heat dissipation end of the semiconductor refrigeration plate, by using internal compression rods to provide elastic tension potential energy, by using self-tapping screw heads to screw together with the internal guide rod threads, by using lower supporting beams to bear pressure on the lower end of the neutral rod, by using internal pressure holding springs to bear the pressure of the two groups of force-bearing compression rods.

[0033] After adopting the above technical solution, the beneficial effect of the method is: after the signal receiver receives the operation control instruction transmitted by the remote controller by using the controller, the control instruction is compiled by the controller, and the power of the flat motor and the side motor is controlled according to the operation control instruction transmitted by the remote controller;

[0034] By using the speed sensing module, power control module, image acquisition module, satellite positioning module, level detection module and height sensing module, the numerical information detected by each module is transmitted to the remote controller through the signal transceiver module and displayed on the digital display screen. BRIEF DESCRIPTION OF THE DRAWINGS

[0035] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative labor.

[0036] Figure 1 This is a schematic diagram of the front top view of a UAV control device of the present invention;

[0037] Figure 2 This is a schematic diagram of the front side top view of the power rotor blade in a UAV control device of the present invention;

[0038] Figure 3 This is a schematic diagram of the front side top view of the structure of the side collection component of a drone control device of the present invention;

[0039] Figure 4 This is a schematic diagram of a front plan view of the upper end portion of a lower support seat in a drone control device of the present invention;

[0040] Figure 5 This is a schematic diagram of the front side top view of the base and the lower sealing ring in a drone control device of the present invention;

[0041] Figure 6 This is a schematic diagram of the front side top view of the lower end portion of the lower embedded sealing ring in a drone control device of the present invention;

[0042] In the figure: 1-power rotor, 2-flat motor, 3-inner support frame, 4-adjustment support frame, 5-adjustment assembly, 6-side collection component, 7-main body, 8-signal transceiver module, 9-lower support seat;

[0043] 51-inner movable shaft, 52-lower support seat, 53-connecting embedded tail, 54-embedded seat

[0044] 61-camera embedded shell, 62-horizontal rotating seat, 63-mounting frame, 64-axial rotating column, 65-side motor, 66-lower supporting frame, 67-internal embedded gear, 68-lower movable embedded seat;

[0045] 91-lower heat dissipation support, 92-heat dissipation slot, 93-embedded slot, 94-semiconductor cooling plate, 95-support foot, 96-inner spring seat rod, 97-lower embedded seat, 98-self-tapping rotary head, 99-inner compression rod, 901-base, 902-lower embedded sealing ring;

[0046] 9a-upper guide seat, 9b-force bearing rod, 9c-external support rod, 9d-internal pressure holding spring, 9e-internal force guiding rod, 9f-internal movable groove one, 9g-internal movable groove two, 9h-supporting beam, 9i-neutral rod. DETAILED DESCRIPTION

[0047] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0048] See also Figure 1-Figure 6 , a UAV control device, comprising: a power rotor blade 1, an adjustment component 5, a side collection component 6 and a lower support seat 9, the power rotor blade 1 is provided with six groups, and the six groups of power rotor blades 1 are evenly distributed on the outside of the main body in an annular structure;

[0049] A group of flat motors 2 for providing power to the power rotors 1 are provided at the lower end of each group of power rotors 1, a group of inner support frames 3 for limiting and connecting the outer side of the flat motors 2 are provided, and a group of support ring seats for providing support effects with the inner support frames 3 are provided on the outer side of the inner support frames 3;

[0050] The support ring seat is a hollow structure, and a group of air cavities for upward air circulation are provided inside the support ring seat. The cross-section of the support ring seat when viewed from above is a circular structure. A group of adjustment brackets 4 for supporting the lower end of the support ring seat are provided on the right side of the support ring seat. The support ring seat can provide a supporting effect together with the internal support frame 3, and the lower end of the support ring seat can be supported by using the adjustment brackets 4.

[0051] A set of adjustment components 5 for adjusting the height of the adjustment support 4 and the power rotor blade 1 is provided on the inner side of the right side of the adjustment support 4, and a main body 7 is provided on the inner side of several sets of adjustment components 5;

[0052] A group of signal transceiver modules 8 for performing signal receiving and sending functions are provided at the upper end of the main body 7. The signal transceiver module 8 is an integral structure with the main body 7, and a group of electric telescopic rods for adjusting the height of the signal transceiver module 8 are provided at the lower end of the main body 7. A group of lower support seats 9 for slowly releasing support for the lower end of the main body 7 are provided at the lower end of the main body 7. The lower support seat 9 is a movable mechanism.

[0053] As the first embodiment of the present invention, when the staff operates the UAV to perform flight operations on rainy days, since the main body 7 has a circular cross-section when viewed from above, a group of waterproof shells for protecting the interior thereof are provided on the outside of the main body 7, and a group of rubber sealing rings are provided at the connection between the waterproof shell and the main body 7. The height of the signal transceiver module 8 is adjusted by using an electric telescopic rod, thereby expanding the signal reception and transmission range to eliminate the poor control signal on rainy days. At the same time, the waterproof shell is used to protect the interior of the main body 7, and the rubber sealing ring can be used to prevent water from penetrating into the interior of the main body 7.

[0054] A group of control combination sensor modules for controlling signal reception and transmission are provided inside the main body 7. The control combination sensor modules include a speed sensor module, a power control module, a picture acquisition module, a satellite positioning module, a level detection module, a height sensor module and a controller. The speed sensor module, the power control module, the picture acquisition module, the satellite positioning module, the level detection module and the height sensor module are all connected to the controller through wires.

[0055] The adjustment assembly 5 includes an inner movable shaft 51 and an insert seat 54. The left side of the inner movable shaft 51 and the right side of the adjustment support frame 4 are sleeved and fixed to each other.

[0056] A group of small servo motors are arranged outside the inner movable shaft 51 to drive the inner movable shaft 51 to rotate actively. The driving end of the small servo motor is connected to the inner movable shaft 51. A group of lower support platforms 52 are arranged on the upper end of the inner movable shaft 51 to provide support for the inner movable shaft 51. The cross section of the lower support platform 52 is an L-shaped structure.

[0057] As the second embodiment of the present invention: since the lower support platform 52 is made of a metal material, a group of connecting domes 53 for providing a connecting support effect for the lower support platform 52 is provided at the upper end of the lower support platform 52, the connecting domes 53 and the lower support platform 52 are an integral forging structure, the lower support platform 52 and the embedding seat 54 are mutually embedded and connected, the cross-section of the embedding seat 54 is a concave structure, and the embedding seat 54 and the lower support platform 52 are movably connected through a group of shafts, the embedding seat 54 and the main body 7 are an integral structure, the lower support platform 52 can be used to provide a supporting effect for the inner movable shaft 51, and the lower connecting domes 53 can be used to provide a connecting support effect for the lower support platform 52.

[0058] The side acquisition component 6 includes a camera housing 61 and a lower movable housing 68. The right side cross section of the camera housing 61 is a ring structure. A group of camera bodies for acquiring images from the lower end of the main body 7 are arranged inside the camera housing 61.

[0059] A set of horizontal rotating seats 62 for horizontally rotating the camera embedded housing 61 is provided at the lower end of the camera embedded housing 61, a set of mounting frames 63 for supporting the horizontal rotating seats 62 is provided at the lower end of the horizontal rotating seats 62, a set of axial rotating posts 64 for driving the camera embedded housing 61 to flip up and down are provided on the front side of the mounting frames 63, a set of side motors 65 for flipping the camera embedded housing 61 left and right are provided on the front side of the axial rotating posts 64, and a set of outer embedded housings for limiting the movement of the side motors 65 are provided on the outer side of the side motors 65;

[0060] The cross-section of the outer embedded shell is an inverted U-shaped structure. A group of lower support frames 66 for supporting the outer embedded shell are provided at the lower end of the outer embedded shell. The lower support frame 66 and the outer embedded shell are fixed by two groups of bolts. A group of lower movable seats 68 for mutual engagement with the main body 7 are provided at the lower right end of the lower support frame 66. A group of inner teeth 67 for maintaining directional movement of the lower support frame 66 are provided on the right side of the lower support frame 66. A group of adjusting gears for actively adjusting the forward and backward movement of the lower support frame 66 are provided on the right side of the inner teeth 67. The adjusting gears are meshed with the inner teeth 67. The lower support frame 66 can be used to support the outer embedded shell, the lower movable seat 68 can be used to be movably engaged with the main body 7, the inner teeth 67 can be used to maintain directional movement of the lower support frame 66, and the adjusting gears can be used to actively adjust the forward and backward movement of the lower support frame 66.

[0061] The lower support seat 9 includes a lower heat dissipation support 91 and a lower sealing ring 902. The cross section of the lower support seat 9 is a circular structure when viewed from above. The lower support seat 9 is a movable structure, and the upper end of the lower support seat 9 is connected to the lower end of the main body 7 through a plurality of groups of air damping rods.

[0062] A group of semiconductor cooling plates 94 for actively cooling the interior of the main body 7 are provided in the middle of the lower end thereof. The upper end of the semiconductor cooling plate 94 is a cooling end, and the lower end of the semiconductor cooling plate 94 is a heat dissipation end. A group of embedded grooves 93 for limiting the installation of the semiconductor cooling plate 94 are provided on the outer side thereof.

[0063] As the third embodiment of the present invention: when the control combination sensor module inside the main body 7 is used for a long time, the main body 7 will generate a high amount of heat. Since a group of semiconductor cooling sheets 94 for actively cooling the inside of the main body 7 are provided in the middle of the lower end of the main body 7, the upper end of the semiconductor cooling sheet 94 is a cooling end, and the cooling end is kept in contact with the main body 7, and can continuously provide a cooling effect for the main body 7. At the same time, since a group of lower heat dissipation supports 91 for conducting heat to the heat dissipation end of the semiconductor cooling sheet 94 are provided on the outer side of the embedded groove 93, the cross section of the lower heat dissipation support 91 when viewed from above is a ring -shaped structure, the lower heat dissipation support 91 is made of an aluminum alloy material, and a plurality of heat dissipation grooves 92 for ventilating the heat dissipation end of the semiconductor refrigeration sheet 94 are dispersedly arranged inside the lower heat dissipation support 91. The semiconductor refrigeration sheet 94 can be used to actively cool the inside of the main body 7, and the lower heat dissipation support 91 can be used to conduct heat to the heat dissipation end of the semiconductor refrigeration sheet 94. The heat dissipation grooves 92 can be used to ventilate the heat dissipation end of the semiconductor refrigeration sheet 94, so as to ensure that the semiconductor refrigeration sheet 94 can continue to provide a cooling effect when the main body 7 is used for a long time.

[0064] Several groups of heat dissipation grooves 92 are distributed in an annular structure, and the interiors of several groups of heat dissipation grooves 92 are interconnected with the interiors of the embedded grooves 93. Four groups of support feet 95 for positioning and installing the lower heat dissipation support 91 are provided at the lower end of the lower heat dissipation support 91;

[0065] Each set of supporting feet 95 is provided with a set of inner spring seat rods 96 for pressing and fitting therewith, and the lower end of the inner spring seat rods 96 is provided with a set of self-tapping screw heads 98 for screwing with the inner force guide rods 9e, and the inner part of the inner spring seat rods 96 is provided with a set of inner compression rods 99 for providing elastic tension potential energy;

[0066] The inner compression rod 99 is a pneumatic damping rod. The lower end of the inner compression rod 99 is provided with a base 901 for supporting its bottom. The lower end of the base 901 is provided with a lower embedded sealing ring 902 for sealing and embedding connection with the lower embedded seat 97. The inner compression rod 99 can provide elastic tension potential energy and can be screwed together with the inner guide rod 9e thread by using a self-tapping screw head 98.

[0067] The lower support seat 9 also includes an upper guide seat 9a, an inner movable groove 9g, a support beam 9h and a neutral rod 9i. The upper guide seat 9a has a ring-shaped cross section when viewed from above. A group of external support rods 9c are provided at the lower ends of the left and right sides of the upper guide seat 9a for supporting the lower end thereof.

[0068] A group of pressure rods 9b for bearing the pressure of the lower end of the lower embedded seat 97 are provided at both left and right ends of the inner side of the upper guide seat 9a. The lower ends of the two groups of pressure rods 9b are movably connected by shafts, and a group of neutral rods 9i for transmitting the pressure of the two groups of pressure rods 9b are provided inside the lower ends of the two groups of pressure rods 9b.

[0069] A group of lower supporting beams for bearing pressure on the lower end of the neutral rod 9i are provided at the lower end, and the left and right sides of the lower supporting beams are connected and fixed with the two groups of external support rods 9c. A group of internal pressure holding springs 9d for bearing pressure are provided at the lower end of the middle position of the two groups of force-bearing pressure rods 9b, and a group of internal movable grooves 1 9f and 2 9g for guiding the moving positions of the two groups of force-bearing pressure rods 9b are provided at the left and right ends of the inner side of the internal pressure holding springs 9d;

[0070] The inner movable groove 1 9f and the inner movable groove 2 9g have the same specifications, and the inner movable groove 1 9f is arranged on the left side, and the inner movable groove 2 9g is arranged on the right side. The lower end of the inner pressure holding spring 9d is provided with a group of supporting beams 9h for supporting its lower end. The supporting beams 9h are a fixed structure and are connected and fixed to the lower end of the inner pressure holding spring 9d. By using the lower supporting beam, the lower end of the neutral rod 9i can be subjected to pressure, and the pressure of the two groups of force-bearing pressure rods 9b can be subjected to pressure by using the inner pressure holding spring 9d.

[0071] As the fourth embodiment of the present invention: when the present invention is falling, its lower support seat 9 contacts with the ground and provides support, and the gravity generated by its main body 7 is squeezed downward by the internal compression rod 99, and the two groups of force-bearing pressure rods 9b are pressed inside the upper guide seat 9a through the base 901 and the lower embedded ring 902. After the two groups of force-bearing pressure rods 9b are subjected to pressure, they move downward along the inner movable groove 1 9f and the inner movable groove 2 9g, and the two groups of force-bearing pressure rods 9b squeeze the inner pressure holding spring 9d for compression, thereby relieving the pressure on the main body 7. At the same time, since a group of supporting beams 9h for supporting the lower end of the inner pressure holding spring 9d is provided at the lower end thereof, the supporting beam 9h is a fixed structure and is connected and fixed to the lower end of the inner pressure holding spring 9d. By using the lower supporting beam, the lower end of the neutral rod 9i can be pressed to ensure the stability of the center of gravity of the lower support seat 9.

[0072] A method for controlling a drone, firstly, a staff member transmits an operation control instruction by using a remote controller, and after a signal receiver receives the operation control instruction transmitted by the remote controller, the staff member compiles the control instruction by the controller, and performs power control on a flat motor 2 and a side motor 65 according to the operation control instruction transmitted by the remote controller, thereby controlling the drone, and at the same time, a speed sensing module, a power control module, a picture acquisition module, a satellite positioning module, a level detection module, and a height sensing module inside a main body 7 can convert a digital signal into an analog signal through a digital-to-analog converter integrated inside the controller, and transmit the numerical information detected by each module to the remote controller end through a signal transceiver module 8, and display it through a digital display screen, and can use a controller to transmit the operation control instruction transmitted by the remote controller to a signal receiver, and compile the control instruction by the controller, and perform power control on a flat motor 2 and a side motor 65 according to the operation control instruction transmitted by the remote controller, and can use a speed sensing module, a power control module, a picture acquisition module, a satellite positioning module, a level detection module, and a height sensing module to transmit the numerical information detected by each module to the remote controller end through a signal transceiver module 8, and display it through a digital display screen.

[0073] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A drone control device, comprising: The power rotor blades (1), the adjustment assembly (5), the side collection component (6) and the lower support seat (9) are characterized in that: the power rotor blades (1) are provided in six groups, and the six groups of the power rotor blades (1) are in an annular structure and are evenly distributed on the outside of the main body; A group of flat motors (2) for providing power to the power rotor blades (1) are provided at the lower end of each group of the power rotor blades (1); a group of inner support frames (3) for limiting and connecting the outer sides of the flat motors (2) are provided on the outer sides thereof; and a group of support ring seats for providing support effects with the inner support frames (3) are provided on the outer sides of the inner support frames (3); The support ring seat is a hollow structure, and a group of air cavities for circulating air upward are arranged inside the support ring seat. The cross section of the support ring seat when viewed from above is a circular structure. A group of adjustment brackets (4) for supporting the lower end of the support ring seat are arranged on the right side of the support ring seat.

2. The drone control device according to claim 1, characterized in that: A group of adjustment components (5) for adjusting the height of the adjustment support (4) and the power rotor (1) are provided on the inner side of the right side of the adjustment support (4), and a main body (7) is provided on the inner side of a plurality of groups of the adjustment components (5); A group of signal transceiver modules (8) for performing signal transceiver functions are provided at the upper end of the main body (7); the signal transceiver modules (8) and the main body (7) are in an integrated structure; a group of electric telescopic rods for adjusting the height of the signal transceiver modules (8) are provided at the lower end of the signal transceiver modules (8); and a group of lower support seats (9) for slowly releasing the lower end of the main body (7) are provided at the lower end of the main body (7); The lower support seat (9) is a movable mechanism. The main body (7) has a circular structure in cross section when viewed from above. A group of waterproof shells for protecting the interior of the main body (7) are provided on the outside of the main body (7). A group of rubber sealing rings are provided at the connection between the waterproof shell and the main body (7).

3. The drone control device according to claim 2, characterized in that: A group of control combination sensor modules for controlling signal reception and transmission are arranged inside the main body (7), and the control combination sensor modules include a speed sensor module, a power control module, a picture acquisition module, a satellite positioning module, a level detection module, a height sensor module and a controller. The speed sensor module, the power control module, the picture acquisition module, the satellite positioning module, the level detection module and the height sensor module are all connected to the controller through wires.

4. The drone control device according to claim 2, characterized in that: The adjustment component (5) comprises an inner movable shaft (51) and an insert seat (54), and the left side of the inner movable shaft (51) and the right side of the adjustment support frame (4) are mutually sleeve-connected and fixed; A group of small servo motors for driving the inner movable shaft (51) to rotate actively are arranged on the outer side of the inner movable shaft (51); a driving end of the small servo motor is connected to the inner movable shaft (51) by power; a group of lower support platforms (52) for providing support to the inner movable shaft (51) are arranged on the upper end of the inner movable shaft (51); and a cross section of the lower support platform (52) is arranged in an L-shaped structure; The lower support platform (52) is made of a metal material. A group of connecting dowels (53) for providing a connecting and supporting effect for the lower support platform (52) is provided at the upper end of the lower support platform (52). The connecting dowels (53) and the lower support platform (52) are an integral forging structure. The lower support platform (52) and the insert seat (54) are mutually engaged and connected. The cross section of the insert seat (54) is a concave structure. The insert seat (54) and the lower support platform (52) are movably connected via a group of shafts. The insert seat (54) and the main body (7) are an integral structure.

5. The drone control device according to claim 2, characterized in that: The side acquisition component (6) comprises a camera housing (61) and a lower movable housing (68); the right side cross section of the camera housing (61) is an annular structure; a group of camera bodies for acquiring images from the lower end of the main body (7) are arranged inside the camera housing (61); A group of horizontal rotating seats (62) for horizontally rotating the camera housing (61) are provided at the lower end of the camera housing (61); a group of mounting frames (63) for supporting the horizontal rotating seats (62) are provided at the lower end; a group of axial rotating columns (64) for driving the camera housing (61) to flip up and down are provided on the front side of the mounting frames (63); a group of side motors (65) for flipping the camera housing (61) left and right are provided on the front side of the axial rotating columns (64); and a group of outer housings for limiting the movement of the side motors (65) are provided on the outer side of the side motors (65); The cross section of the outer embedded shell is an inverted U-shaped structure. A group of lower support frames (66) for supporting the outer embedded shell are provided at the lower end of the outer embedded shell. The lower support frame (66) and the outer embedded shell are connected and fixed by two groups of bolts. A group of lower movable embedding seats (68) for mutual engagement with the main body (7) are provided at the lower right end of the lower support frame (66). A group of inner embedded teeth (67) for maintaining directional movement of the lower support frame (66) are provided on the right side. A group of adjusting gears for actively adjusting the forward and backward movement of the lower support frame (66) are provided on the right side of the inner embedded teeth (67). The adjusting gears are meshed with the inner embedded teeth (67).

6. The drone control device according to claim 2, characterized in that: The lower support seat (9) comprises a lower heat dissipation support (91) and a lower sealing ring (902); the cross section of the lower support seat (9) is a circular structure when viewed from above; the lower support seat (9) is a movable structure; and the upper end of the lower support seat (9) is connected to the lower end of the main body (7) via a plurality of groups of air damping rods; A group of semiconductor cooling sheets (94) for actively cooling the interior of the main body (7) are provided at the middle position of the lower end of the main body (7); the upper end of the semiconductor cooling sheet (94) is a cooling end, the lower end of the semiconductor cooling sheet (94) is a heat dissipation end, and a group of embedded grooves (93) for limiting the installation of the semiconductor cooling sheet (94) are provided on the outer side of the semiconductor cooling sheet (94); A group of lower heat dissipation supports (91) for conducting heat to the heat dissipation end of the semiconductor cooling plate (94) are arranged on the outside of the embedded groove (93); the cross section of the lower heat dissipation support (91) is an annular structure when viewed from above; the lower heat dissipation support (91) is made of an aluminum alloy material; and a plurality of groups of heat dissipation grooves (92) for ventilating the heat dissipation end of the semiconductor cooling plate (94) are dispersedly arranged inside the lower heat dissipation support (91).

7. The drone control device according to claim 6, characterized in that: The plurality of groups of heat dissipation grooves (92) are distributed in an annular structure, the interiors of the plurality of groups of heat dissipation grooves (92) are interconnected with the interiors of the embedded grooves (93), and the lower end of the lower heat dissipation support (91) is provided with four groups of support feet (95) for positioning and installing the lower heat dissipation support (91); A group of inner spring seat rods (96) for pressing and engaging with the outer side of each group of support legs (95) is provided inside, a group of self-tapping screw heads (98) for screwing with the inner force guide rods (9e) are provided at the lower ends of the inner spring seat rods (96), and a group of inner compression rods (99) for providing elastic tension potential energy are provided inside the inner spring seat rods (96); The inner compression rod (99) is a pneumatic damping rod. The lower end of the inner compression rod (99) is provided with a group of bases (901) for supporting the bottom thereof. The lower end of the base (901) is provided with a group of lower embedding rings (902) for sealingly embedding and connecting the lower embedding seat (97).

8. The drone control device according to claim 7, characterized in that: The lower support seat (9) further comprises an upper guide seat (9a) and a neutral rod (9i); the upper guide seat (9a) has a ring-shaped cross-section when viewed from above, and a group of external support rods (9c) for supporting the lower end of the upper guide seat (9a) are provided at the lower ends of the left and right sides; A group of pressure rods (9b) for bearing the pressure of the lower end of the lower embedded seat (97) are provided at both left and right ends of the inner side of the upper guide seat (9a), the lower ends of the two groups of pressure rods (9b) are movably connected by shafts, and a group of neutral rods (9i) for transmitting the pressure borne by the two groups of pressure rods (9b) are provided on the inner sides of the lower ends of the two groups of pressure rods (9b); The lower end of the neutral rod (9i) is provided with a group of lower supporting beams for bearing pressure on the lower end thereof, and the left and right sides of the lower supporting beams are both connected and fixed to the two groups of outer supporting rods (9c), and the lower ends of the middle positions of the two groups of pressure rods (9b) are provided with a group of inner pressure holding springs (9d) for bearing pressure thereon, and the left and right ends of the inner side of the inner pressure holding springs (9d) are both provided with a group of inner movable grooves 1 (9f) and 2 (9g) for guiding the moving positions of the two groups of pressure rods (9b); The inner movable groove 1 (9f) and the inner movable groove 2 (9g) have the same specifications, and the inner movable groove 1 (9f) is arranged on the left side, and the inner movable groove 2 (9g) is arranged on the right side. The lower end of the inner pressure holding spring (9d) is provided with a group of supporting beams (9h) for supporting the lower end thereof. The supporting beams (9h) are a fixed structure and are connected and fixed to the lower end of the inner pressure holding spring (9d).

9. A method for controlling a drone using any one of claims 1 to 8, characterized in that: The method comprises the following steps: firstly, a staff member transmits an operation control instruction by using a remote controller, and after receiving the operation control instruction transmitted by the remote controller, the signal receiver compiles the control instruction through the controller, and controls the power of the flat motor (2) and the side motor (65) according to the operation control instruction transmitted by the remote controller, thereby controlling the unmanned aerial vehicle. At the same time, the speed sensing module, power control module, image acquisition module, satellite positioning module, level detection module, and height sensing module inside the main body (7) can convert digital signals into analog signals through the digital-to-analog converter integrated inside the controller, and transmit the numerical information detected by each module to the remote controller end through the signal transceiver module (8), and display it through the digital display screen.

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