CN112319807B

CN112319807B - Unmanned aerial vehicle control platform control method based on intelligent equipment

Info

Publication number: CN112319807B
Application number: CN202011263466.2A
Authority: CN
Inventors: 何永钟; 李佳敏; 李育平; 王荣远; 郑先亮; 邱微
Original assignee: Guangdong United Jindi Real Estate Appraisal Survey And Design Co ltd
Current assignee: Guangdong United Jindi Real Estate Appraisal Survey And Design Co ltd
Priority date: 2020-11-12
Filing date: 2020-11-12
Publication date: 2022-05-10
Anticipated expiration: 2040-11-12
Also published as: CN112319807A

Abstract

The utility model can be applied to the technical field of unmanned aerial vehicle aerial survey and natural resource sanitary film enforcement and patrol, and particularly relates to an unmanned aerial vehicle control platform control method based on intelligent equipment. The utility model solves the problems that the existing unmanned aerial vehicle has short endurance time and the transmission of the signal of the monitoring graph of the unmanned aerial vehicle only stays in the range of 5-7 km. The method is a better solution to the problems that the field image cannot be acquired in real time once the range is exceeded, the information transmission distance is short, the specific position of the airplane is grasped, and the like.

Description

Unmanned aerial vehicle control platform control method based on intelligent equipment

Technical Field

The utility model belongs to the field of unmanned aerial vehicle aerial survey and natural resource satellite law enforcement and patrol, and particularly relates to a control method of an unmanned aerial vehicle control platform based on intelligent equipment.

Background

Unmanned vehicles aerial survey and natural resource satellite law enforcement patrol are important components for providing technical support for the unmanned vehicles in natural resource management, can provide the most intuitive reflection for field conditions, is a means for acquiring real data of the earth surface, and is the leading-edge science and technology in the field of surveying and mapping at present. Most of the work of the original field data acquisition is transferred to the indoor space to be finished through the aerial survey of the unmanned aerial vehicle, so that the labor intensity of surveying and mapping engineering technicians is greatly reduced, data with uniform precision and small errors can be provided, and a basis is provided for natural resource management; the natural resource law enforcement and patrol is a normal work of natural resources, an unmanned aerial vehicle patrol system is utilized to discover illegal behaviors of the natural resources in time, and a basis is provided for law enforcement and punishment of the natural resources in the processes of photographing, evidence obtaining and the like.

The publication number is CN207053631U Chinese patent and discloses a road monitoring support, its technical scheme main points are including supporting component and horizontal pole, supporting component includes coaxial coupling's outer tube and pole setting, the one end and the pole setting top fixed connection of horizontal pole, the surface of pole setting is equipped with the external screw thread along its length direction, form the guide way along its generating line direction indent in the pole setting, the outer tube inner wall rotates and is connected with the sleeve pipe, sleeve pipe and pole setting threaded connection, outer tube inner wall both ends are equipped with respectively with guide way complex stopper, the coaxial ring gear that is fixed with in sleeve pipe bottom, the ring gear part exposes outside the outer tube, the ring gear is connected with drive assembly, drive assembly includes positive and negative motor, fix at motor output shaft tip and with the gear ring meshing's gear. The utility model solves the problem of potential safety hazard in the high-altitude installation of the existing unmanned aerial vehicle camera.

However, the above patents do not solve the problems that the aerial photographing operation of the unmanned aerial vehicle in the market is mostly operated through a radio station, the transmission of the image transmission signal only stays in the range of 5-7 kilometers, the field image cannot be obtained in real time once the field image is out of the range, the specific position of the aircraft is mastered, the state of the aircraft can be judged only through the data transmission signal, the aircraft is not visual enough, the electric power endurance is insufficient, the requirement of long-time flight operation cannot be met, and the aerial photographing dead angle of the existing unmanned aerial vehicle is too many.

Disclosure of Invention

Aiming at the defects in the prior art, the utility model provides an unmanned aerial vehicle control platform based on intelligent equipment, which is used for solving the problems that in the prior art, the transmission of image signaling signals only stops in the range of 5-7 kilometers, the field image cannot be acquired in real time once the transmission exceeds the range, the specific position of the aircraft is mastered, the state of the aircraft can be judged only through data transmission signals, the aircraft is not visual enough, the electric power endurance is insufficient, the requirement of long-time flight operation cannot be met, and the existing unmanned aerial vehicle has a large number of aerial dead angles. The utility model also provides an operation method of the unmanned aerial vehicle control platform of the intelligent device, which is convenient for improving the aerial photography efficiency of the unmanned aerial vehicle.

In order to solve the technical problems, the utility model adopts the following technical scheme:

an unmanned aerial vehicle control platform based on intelligent equipment comprises a charging station, a charging mechanism and an unmanned aerial vehicle, wherein the charging mechanism is arranged at the top end of the charging station, and the unmanned aerial vehicle is arranged above the charging mechanism when in a parking state;

when unmanned vehicles stops at charging mechanism, the charging station carries electric power to charging mechanism, unmanned vehicles accessible charges mechanism and carries out the power supply and supply, at this moment, unmanned vehicles driving system stop work, use mobilizable unmanned vehicles to carry out road surveillance camera's work, the continuation of the journey problem that unmanned vehicles is used for the control has been solved, the problem that it is many to use ordinary surveillance camera control dead angle has been solved simultaneously, and set up a plurality of charging stations as unmanned vehicles information transmission receiving platform, cover through the information multiple spot, in time master unmanned vehicles scene real-time image, and master the concrete position that the aircraft was located, improve monitoring efficiency.

Furthermore, the charging station comprises a lighting device, a first charging rod body and a second charging rod body, wherein the tail end of the lighting device is fixedly connected with the top end of the first charging rod body, and the rear section of the first charging rod body penetrates through the upper section of the second charging rod body and is fixedly connected with the second charging rod body;

the charging station further comprises a first fixed cable and a second fixed cable, the top end of the first fixed cable is fixedly connected with the middle section of the first charging rod body, the tail end of the first fixed cable is fixedly connected with the upper section of the second charging rod body, the top end of the second fixed cable and the first charging rod body penetrate through the part of the second charging rod body to be fixedly connected, and the second fixed cable and the upper section of the second charging rod body are fixedly connected.

The lighting device can illuminate the ground at night, when the unmanned aerial vehicle stops, the charging station can charge the unmanned aerial vehicle through the charging mechanism, the charging mechanism can be additionally installed to install a street lamp or a required position meeting requirements, the problem that a common monitor cannot be installed or is installed in a place with low utilization rate and the like which are not in line with economic benefits is solved through the stopped unmanned aerial vehicle, the monitoring dead angle is eliminated, the device is multipurpose, the use cost is greatly reduced, and the monitoring and economic benefits are improved. Furthermore, the unmanned aerial vehicle comprises a four-axis frame, a shell, a signal receiver-transmitter and a flight controller, wherein the four-axis frame is fixedly connected with the shell, the signal receiver-transmitter is arranged at the top of the shell, the flight controller is arranged in front of the signal receiver-transmitter, the bottom of the flight controller is fixedly connected with the top of the shell, the unmanned aerial vehicle also comprises a foot rest component and a monitoring device, the foot rest component is arranged at the bottom of the shell, and the monitoring device is arranged at the rear section of the bottom of the shell;

the foot rest component comprises two groups of connecting foot rests and two groups of auxiliary foot rests, the two groups of connecting foot rests are respectively arranged at the left end and the right end of the bottom of the machine shell, and the two groups of auxiliary foot rests are arranged at the rear end of the bottom of the machine shell;

the connecting foot rest comprises a connecting rod body and a fixing rod body, and the bottom end of the connecting rod body is fixedly connected with the middle section of the fixing rod body;

when unmanned vehicles flight state, two sets of connection foot rests and two sets of supplementary foot rests upwards fold up to 90 degrees, avoid hanging and cause unmanned vehicles to touch foreign matter such as electric wire when flying, when unmanned vehicles stops, two sets of connection foot rests and two sets of supplementary foot rests expand downwards and are triangle-shaped, two sets of connection foot rests can support unmanned vehicles, two sets of supplementary foot rests guarantee that unmanned vehicles can not direct contact ground and cause unmanned vehicles to damage when central skew appears in unmanned vehicles bottom surface descending, when unmanned vehicles stops the charging station, two sets of connection foot rests and two sets of supplementary foot rests expand downwards and are triangle-shaped, spacing sliding block tightens up to spacing sliding shaft direction and carries on spacingly to the connecting rod body, after the connection is accomplished, the mechanism of charging charges unmanned vehicles through connecting the foot rest.

Further, the fixed body of rod includes body of rod body, the body of rod presss from both sides tight piece, focus regulating block, the body of rod presss from both sides tight piece and has two the body of rod presss from both sides tight piece and locates about body of rod body middle section respectively, focus regulating block has two, two both ends about the body of rod is located respectively to the focus regulating block.

When unmanned vehicles berths, the body of rod body is with when the structure contact that charges, the body of rod presss from both sides tight piece and can press from both sides tightly spacing sliding block, guarantee the stability that unmanned vehicles connects, make unmanned avoiding because factor disconnection such as wind-force when charging, cause unmanned vehicles to damage, when unmanned vehicles prepares to take off, the body of rod presss from both sides tight piece and slides to body of rod body both sides, release first sliding block and second sliding block, it is fixed with unmanned vehicles to release first sliding block and second sliding block release, the foot rest component upwards folds up 90 degrees, unmanned vehicles takes off.

Further, the monitoring device comprises a suspension holder and a camera, and the camera is arranged at the front end of the suspension holder;

the suspension holder comprises a first suspension fixing table, a first suspension arm and a second rotation fixing table, the bottom of the first suspension fixing table is connected with the top end of the first suspension arm, and the tail end of the first suspension arm is connected with the right part of the second rotation fixing table;

the suspension holder also comprises a second suspension arm, the tail end of the second suspension arm is fixedly connected with the camera, and the head end of the second suspension arm is connected with the left part of the second rotary fixed table;

through many spiral arms and many revolving stages, make unmanned vehicles's monitored control system when bottom surface or aerial control, can furthest's performance monitoring effect, the control is more comprehensive, and the control does not have the dead angle, makes unmanned vehicles ' work efficiency improve, and the work precision improves greatly.

Further, the four-axis frame includes paddle, rotation axis and connecting axle, the paddle is installed at the rotation axis upper end and rather than swing joint, the rotation axis passes through connecting axle and casing fixed connection.

Improve unmanned vehicles's equipment strength and flight work efficiency through the four-axis frame, make unmanned vehicles can arrive appointed place more fast, use the signal to receive simultaneously and send out ware and flight controller, improve unmanned vehicles's flight smoothness and data transmission return speed, make unmanned returning to the journey more accurate, unexpected trouble appearance rate reduces greatly.

Further, the signal receiver comprises an alarm module, a wireless positioning tag, a manual correction module and a position correction module;

the alarm module alarms when the unmanned aerial vehicle deviates from a preset coordinate threshold range, and starts automatic position correction;

the wireless positioning tag receives positioning radio waves sent by the ground station and replies a wireless pulse signal;

and the manual correction module is used for correcting the position of the unmanned aerial vehicle when the unmanned aerial vehicle loses the automatic position correction capability.

And the position correction module corrects the position of the unmanned aerial vehicle according to the three-dimensional coordinate information.

Further, the charging mechanism comprises a charging upper part and a charging lower part, and the charging upper part is arranged above the charging lower part;

the charging upper part comprises a charging seat, a limiting sliding shaft and a limiting sliding block, the inner section of the limiting sliding shaft is arranged in the charging seat, the outer end of the limiting sliding shaft protrudes out of the side part of the charging seat, and the limiting sliding shaft is connected with the limiting sliding block;

the limiting sliding shaft comprises a first sliding shaft and a second sliding shaft, the first sliding shaft is arranged at the right section inside the charging seat, and the second sliding shaft is arranged at the left section inside the charging seat;

the limiting sliding block comprises a first sliding block and a second sliding block, the bottom of the first sliding block is movably connected with the left end of the first sliding shaft, and the bottom of the second sliding block is movably connected with the right end of the second sliding shaft;

charging upper portion carries out mechanical fastening to unmanned vehicles through spacing sliding shaft, spacing sliding block, guarantees the life and the structural strength of equipment, avoids appearing the fixed problem of mistake when unmanned vehicles descends.

Furthermore, the charging station also comprises a wireless positioning base station and a ground station;

the wireless positioning base station captures the wireless pulse signal and sends the information of the wireless pulse signal and the time point thereof to the ground station;

and the ground station processes the wireless pulse signals and the information of the time points thereof into three-dimensional coordinate information of the unmanned aerial vehicle relative to the first base station, and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time.

The unmanned aerial vehicle enters the range of the wireless positioning base station, the wireless positioning tag receives positioning radio waves sent by the ground station and replies a wireless pulse signal, the wireless positioning base station captures the wireless pulse signal and sends the wireless pulse signal and information of the time point of the wireless pulse signal to the ground station, the ground station processes the wireless pulse signal and the information of the time point of the wireless pulse signal into three-dimensional coordinate information of the unmanned aerial vehicle relative to the first base station and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time, and the unmanned aerial vehicle corrects the position of the unmanned aerial vehicle through the three-dimensional coordinate information to complete landing. A wireless positioning tag of the unmanned aerial vehicle receives positioning radio waves sent by a ground station and replies a wireless pulse signal; the wireless positioning base station captures the wireless pulse signal and sends the information of the wireless pulse signal and the time point thereof to the ground station; the ground station processes the wireless pulse signals and the information of the time points of the wireless pulse signals into three-dimensional coordinate information of the unmanned aerial vehicle relative to the first base station, and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time; the unmanned aerial vehicle corrects the position of the unmanned aerial vehicle through the three-dimensional coordinate information to finish take-off, the technical problem that the positioning is inaccurate in the take-off and landing stages of the unmanned aerial vehicle is solved, and the unmanned aerial vehicle is low in cost, high in applicability, high in anti-interference capacity and accurate in positioning.

The operation method of the unmanned aerial vehicle control platform based on the intelligent device comprises the following specific steps:

s1, stopping equipment, wherein the equipment comprises a charging station, a charging mechanism and an unmanned aerial vehicle, the charging mechanism is installed at the top end of the charging station, the unmanned aerial vehicle is arranged above the charging mechanism when in a stopping state, the charging station transmits electric power to the charging mechanism when the unmanned aerial vehicle stops on the charging mechanism, the unmanned aerial vehicle can carry out power supply supplement through the charging mechanism, and at the moment, a power system of the unmanned aerial vehicle stops working;

s2, monitoring the road surface, wherein the monitoring device comprises a suspension holder and a camera, and the camera is arranged at the front end of the suspension holder; the suspension holder comprises a first suspension fixing table, a first suspension arm and a second rotation fixing table, the bottom of the first suspension fixing table is connected with the top end of the first suspension arm, and the tail end of the first suspension arm is connected with the right part of the second rotation fixing table; the suspension holder also comprises a second suspension arm, the tail end of the second suspension arm is fixedly connected with the camera, the head end of the second suspension arm is connected with the left part of the second rotary fixing table, when the unmanned aerial vehicle is in a parking state, the power system of the unmanned aerial vehicle stops working and stops working, a monitoring device is used for monitoring roads on the road surface, energy consumption and equipment loss are reduced, meanwhile, the monitoring device can be used for carrying out maneuvering monitoring according to road sections which are blocked or have serious violation, and monitoring cost is saved;

s3, preparing for taking off of equipment, wherein the first sliding block comprises a first clamping groove and a first connecting shaft, the first clamping groove is formed in the inner side of the first sliding block, the outer section of the first connecting shaft is arranged in the lower section of the first sliding block, and the inner section of the first connecting shaft is arranged in the first sliding block; the second sliding block comprises a second clamping groove and a second connecting shaft, the second clamping groove is arranged on the inner side of the second sliding block, the outer section of the second connecting shaft is arranged in the lower section of the second sliding block, the inner section of the second connecting shaft is arranged in the second sliding block, the first connecting shaft and the second connecting shaft are released to pop out outwards after the first sliding shaft and the second sliding shaft pop out outwards, and the first clamping groove and the second clamping groove do not limit the unmanned aerial vehicle any more;

s4, preparing a second device for takeoff, wherein the fixed rod body comprises a rod body, two rod body clamping blocks and two gravity center adjusting blocks, the two rod body clamping blocks are arranged on the left and right of the middle section of the rod body respectively, the two gravity center adjusting blocks are arranged on the left and right ends of the rod body respectively, the rod body clamping blocks slide towards the two sides of the rod body, the first sliding block and the second sliding block are released from being fixed with the unmanned aerial vehicle, the foot rest component is folded upwards by 90 degrees, and the unmanned aerial vehicle takes off;

s5, information transmission, wherein the charging station further comprises a wireless positioning base station and a ground station; the wireless positioning base station captures the wireless pulse signal and sends the information of the wireless pulse signal and the time point thereof to the ground station; the signal receiver comprises an alarm module, a wireless positioning tag, a manual correction module and a position correction module; the alarm module alarms when the unmanned aerial vehicle deviates from a preset coordinate threshold range, and starts automatic position correction; the wireless positioning tag receives positioning radio waves sent by the ground station and replies a wireless pulse signal; the manual correction module is used for correcting the position of the unmanned aerial vehicle when the unmanned aerial vehicle loses the automatic position correction capability; the position correction module corrects the position of the unmanned aerial vehicle according to the three-dimensional coordinate information; and the ground station processes the wireless pulse signals and the information of the time points thereof into three-dimensional coordinate information of the unmanned aerial vehicle relative to the ground station, and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time. By judging the strength of the remote control signal received by the signal receiver, when the strength of the remote control signal received by the signal receiver is lower than a set threshold value, the unmanned aerial vehicle is controlled to approach the ground station according to the position information and the position information of the ground station, so that the unmanned aerial vehicle can be prevented from flying too far to lose control due to improper operation; furthermore, the data interruption time of the position correction module is also judged, when the data transmission interruption time of the position correction module exceeds the preset time, the unmanned aerial vehicle automatically returns, and when the unmanned aerial vehicle loses contact with the ground station, the unmanned aerial vehicle is controlled to fly to the initial takeoff position, so that safety accidents caused by the fact that the unmanned aerial vehicle loses control are prevented, and the safety of the unmanned aerial vehicle is improved; and S6, monitoring the equipment in the air, and monitoring and surveying the air and the ground by the unmanned aerial vehicle after taking off by using the monitoring device, so that the monitoring range is expanded, data can be collected quickly, the unmanned aerial vehicle can arrive at the incident place more quickly, and the unmanned aerial vehicle can be returned to the original charging station or dispatched to stop at the charging station nearby after the air monitoring is completed.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the unmanned aerial vehicle control platform based on the intelligent equipment, when the unmanned aerial vehicle stops at the charging mechanism, the charging station transmits electric power to the charging mechanism, the unmanned aerial vehicle can be supplemented with power through the charging mechanism, at the moment, the power system of the unmanned aerial vehicle stops working, the movable unmanned aerial vehicle is used for working of the road monitoring camera, the problem of cruising of the unmanned aerial vehicle for monitoring is solved, and the problem of more dead angles of monitoring by using a common monitoring camera is solved.

2. According to the unmanned aerial vehicle control platform based on the intelligent equipment, the problem that a common monitor cannot be installed or the utilization rate is low after installation and the like are not in accordance with economic benefits is solved by parking the unmanned aerial vehicle, the monitoring dead angle is eliminated, the unmanned aerial vehicle control platform is multipurpose, the use cost is greatly reduced, and the monitoring and economic benefits are improved.

3. According to the unmanned aerial vehicle control platform based on the intelligent equipment, the monitoring effect can be exerted to the maximum extent when the monitoring system of the unmanned aerial vehicle monitors on the bottom surface or in the air through the multi-rotating arm and the multi-rotating platform, the monitoring is more comprehensive, no dead angle exists in the monitoring, the working efficiency of the unmanned aerial vehicle is improved, and the working accuracy is greatly improved.

4. According to the unmanned aerial vehicle control platform based on the intelligent equipment, the plurality of charging stations are arranged to serve as the unmanned aerial vehicle information transmitting and receiving platform, real-time images of the unmanned aerial vehicle on site are mastered in time through information multi-point coverage, the specific position of the aircraft is mastered, and the aerial photographing efficiency of the unmanned aerial vehicle is improved.

Drawings

FIG. 1 is a schematic structural diagram of an embodiment of an unmanned aerial vehicle control platform based on intelligent equipment according to the utility model;

FIG. 2 is an enlarged view of the portion X in FIG. 1;

FIG. 3 is a schematic view of a partial structure of an embodiment of an unmanned aerial vehicle control platform based on intelligent equipment according to the utility model;

FIG. 4 is a schematic view of a partial structure of an embodiment of an unmanned aerial vehicle control platform based on intelligent devices according to the present invention;

FIG. 5 is a schematic view of a partial structure of an embodiment of an unmanned aerial vehicle control platform based on intelligent devices according to the present invention;

FIG. 6 is a schematic view of a partial structure of an embodiment of an unmanned aerial vehicle control platform based on an intelligent device according to the present invention;

FIG. 7 is an enlarged view of the portion Y in FIG. 6;

fig. 8 is a functional block diagram of an unmanned aerial vehicle control platform based on intelligent equipment.

Reference numerals referred to in the drawings are: a charging station A; lighting device a 1; the first charging rod body a 2; the second charging rod body a 3; a first fixed cable a 4; a second fixed cable a 5; wireless positioning base station a 6; ground station a 7;

a charging mechanism B; a charging upper part B1; a charging cradle B101; a limit sliding shaft B102; a first slide shaft B1021; the second slide shaft B1022; a limit sliding block B103; first slider B1031; the second slider B1032; a charging lower part B2;

an unmanned aerial vehicle C; a four-axis gantry C1; a blade C101; a rotation axis C102; a connecting shaft C103; case C2; a signaling transceiver C3; an alarm module C301; a wireless positioning tag C302; a manual corrective module C303; a position correction module C304; flight controller C4; a foot rest member C5; a connecting foot rest C501; the connecting rod body C5011; a fixed rod body C5012; the rod body C5012 a; a rod body clamping block C5012 b; a center-of-gravity adjusting block C5012C; an auxiliary stand C502; monitoring device C6; a hanging tripod head C601; a first suspension fixing table C6011; a first suspension arm C6012; a second rotation fixing table C6013; a second suspension arm (not shown); camera C602.

Detailed Description

In order that those skilled in the art can better understand the present invention, the following technical solutions are further described with reference to the accompanying drawings and examples.

It should be noted that all the directional indicators (such as up, down, left, right, front, and rear … …) in the embodiment of the present invention are only used to explain the relative position relationship between the components, the movement situation, etc. in a specific posture (as shown in the drawing), and if the specific posture is changed, the directional indicator is changed accordingly.

In addition, the descriptions related to "first", "second", etc. in the present invention are 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 at least one such feature. In addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.

Example one

As shown in fig. 1-8, an unmanned aerial vehicle control platform based on intelligent devices comprises a charging station a, a charging mechanism B and an unmanned aerial vehicle C, wherein the charging mechanism B is installed at the top end of the charging station a, and the unmanned aerial vehicle C is arranged above the charging mechanism B when in a parking state;

when unmanned vehicles C stop on charging mechanism B, charging station A carries electric power to charging mechanism B, unmanned vehicles C accessible charges mechanism B and carries out the power supply and supply, at this moment, unmanned vehicles C driving system stop work, use mobilizable unmanned vehicles to carry out road surveillance camera's work, the continuation of journey problem that unmanned vehicles is used for the control has been solved, the problem that the ordinary surveillance camera control dead angle is many has been solved simultaneously, and set up a plurality of charging stations and regard as unmanned vehicles information transmission receiving platform, through information multiple spot covering, in time master unmanned vehicles scene real-time image, and master the concrete position that the aircraft was located, improve monitoring efficiency.

Preferably, the unmanned aerial vehicle C includes a four-axis frame C1, a case C2, a signal transceiver C3 and a flight controller C4, the four-axis frame C1 is fixedly connected to the case C2, the signal transceiver C3 is mounted on the top of the case C2, the flight controller C4 is disposed in front of the signal transceiver C3, the bottom of the flight controller C4 is fixedly connected to the top of the case C2, the unmanned aerial vehicle C further includes a foot rest member C5 and a monitoring device C6, the foot rest member C5 is mounted at the bottom of the case C2, and the monitoring device C6 is mounted at the rear section of the bottom of the case C2;

the foot stand component C5 comprises two groups of connecting foot stands C501 and two groups of auxiliary foot stands C502, the two groups of connecting foot stands C501 are respectively installed at the left end and the right end of the bottom of the machine shell C2, and the two groups of auxiliary foot stands C502 are installed at the rear end of the bottom of the machine shell C2;

the connecting foot rest C501 comprises a connecting rod body C5011 and a fixing rod body C5012, and the bottom end of the connecting rod body C5011 is fixedly connected with the middle section of the fixing rod body C5012. When unmanned vehicles is in flight state, two groups of connection foot rests C501 and two groups of auxiliary foot rests C502 are folded upwards to 90 degrees, foreign matters such as electric wires are touched when the unmanned vehicles are prevented from being hung, when the unmanned vehicles stop on the bottom surfaces, the two groups of connection foot rests C501 and the two groups of auxiliary foot rests C502 are unfolded downwards to be triangular, the two groups of connection foot rests C501 can support the unmanned vehicles, the two groups of auxiliary foot rests C502 guarantee that the unmanned vehicles cannot directly contact the ground to cause damage to the unmanned vehicles when the unmanned vehicles stop at the charging station A, the two groups of connection foot rests C501 and the two groups of auxiliary foot rests C502 are unfolded downwards to be triangular, the limiting sliding blocks are tightened up to limit sliding shaft directions to limit the connection rod bodies, and after connection is completed, the charging mechanism B charges the unmanned vehicles through the connection foot rests C501.

Preferably, the fixed rod body C5012 includes a rod body C5012a, two rod body clamping blocks C5012b and a center of gravity adjusting block C5012C, the two rod body clamping blocks C5012b are respectively disposed at the left and right of the middle section of the rod body C5012a, the two center of gravity adjusting blocks C5012C are respectively disposed at the left and right ends of the rod body C5012 a. When unmanned vehicles stop, when the body of rod body contacts with the structure of charging, body of rod presss from both sides tight piece C5012B and can press from both sides tight spacing sliding block, guarantee the stability that unmanned vehicles connects, make unmanned avoidance of when charging because factor such as wind-force disconnection, cause unmanned vehicles to damage, when unmanned vehicles prepares to take off, body of rod presss from both sides tight piece C5012B and slides to body of rod both sides, release first sliding block B1031 and second sliding block B1032, it releases and is fixed with unmanned vehicles C to release first sliding block B1031 and second sliding block B1032, the foot rest component folds up 90 degrees, unmanned vehicles takes off.

Preferably, the monitoring device C6 includes a suspension holder C601 and a camera C602, and the camera C602 is disposed at the front end of the suspension holder C601;

the suspension holder C601 comprises a first suspension fixed platform C6011, a first suspension arm C6012 and a second rotation fixed platform C6013, wherein the bottom of the first suspension fixed platform C6011 is connected with the top end of the first suspension arm C6012, and the tail end of the first suspension arm C6012 is connected with the right part of the second rotation fixed platform C6013;

the suspension holder C601 further comprises a second suspension arm, the tail end of the second suspension arm is fixedly connected with the camera C602, and the head end of the second suspension arm is connected with the left part of the second rotary fixing table C6013. Through many spiral arms and many revolving stages, make unmanned vehicles's monitored control system when bottom surface or aerial control, can furthest's performance monitoring effect, the control is more comprehensive, and the control does not have the dead angle, makes unmanned vehicles ' work efficiency improve, and the work precision improves greatly.

Preferably, the four-axis frame C1 comprises a paddle C101, a rotating shaft C102 and a connecting shaft C103, the paddle C101 is mounted at the upper end of the rotating shaft C102 and movably connected with the rotating shaft C102, and the rotating shaft C102 is fixedly connected with the casing through the connecting shaft C103. Improve unmanned vehicles's equipment strength and flight work efficiency through the four-axis frame, make unmanned vehicles can arrive appointed place more fast, use the signal to receive simultaneously and send out ware and flight controller, improve unmanned vehicles's flight smoothness and data transmission return speed, make unmanned returning to the journey more accurate, unexpected trouble appearance rate reduces greatly.

Preferably, the signal receiver C3 comprises an alarm module C301, a wireless positioning tag C302, a manual correction module C303 and a position correction module C304;

the alarm module C301 alarms when the unmanned aerial vehicle deviates from the preset coordinate threshold range, and starts automatic position correction;

the wireless positioning tag C302 receives positioning radio waves sent by the ground station A7 and replies a wireless pulse signal;

and the manual correction module C303 corrects the position of the unmanned aerial vehicle when the unmanned aerial vehicle loses the position automatic correction capability.

And the position correction module C304 corrects the position of the unmanned aerial vehicle according to the three-dimensional coordinate information.

Example two

The present embodiment is performed on the basis of the first embodiment, and mainly describes the structure of the unmanned aerial vehicle control platform charging mechanism based on the intelligent device.

As shown in fig. 1 to 8, an unmanned aerial vehicle control platform based on intelligent devices comprises a charging station a, a charging mechanism B and an unmanned aerial vehicle C, wherein the charging mechanism B is installed at the top end of the charging station a, and the unmanned aerial vehicle C is arranged above the charging mechanism B when in a parking state;

the suspension holder C601 comprises a first suspension fixing platform C6011, a first suspension arm C6012 and a second rotation fixing platform C6013, wherein the bottom of the first suspension fixing platform C6011 is connected with the top end of the first suspension arm C6012, and the tail end of the first suspension arm C6012 is connected with the right part of the second rotation fixing platform C6013;

the suspension holder C601 further comprises a second suspension arm, a tail end of the second suspension arm is fixedly connected with the camera C602, and a head end of the second suspension arm is connected with a left portion of a second rotary fixing table C6013. Through many spiral arms and many revolving stages, make unmanned vehicles's monitored control system when bottom surface or aerial control, can furthest's performance monitoring effect, the control is more comprehensive, and the control does not have the dead angle, makes unmanned vehicles ' work efficiency improve, and the work precision improves greatly.

the alarm module C301 alarms when the unmanned aerial vehicle deviates from a preset coordinate threshold range, and starts automatic position correction;

Preferably, the charging mechanism B includes a charging upper part B1 and a charging lower part B2, and the charging upper part B1 is disposed above the charging lower part B2;

the charging upper part B1 comprises a charging seat B101, a limit sliding shaft B102 and a limit sliding block B103, the inner section of the limit sliding shaft B102 is arranged inside the charging seat B101, the outer end of the limit sliding shaft B102 protrudes out of the side part of the charging seat B101, and the limit sliding shaft B102 is connected with the limit sliding block B103;

the limiting sliding shaft B102 comprises a first sliding shaft B1021 and a second sliding shaft B1022, the first sliding shaft B1021 is arranged at the right section inside the charging seat B101, and the second sliding shaft B1022 is arranged at the left section inside the charging seat B101;

the limit sliding block B103 comprises a first sliding block B1031 and a second sliding block B1032, wherein the bottom of the first sliding block B1031 is movably connected with the left end of a first sliding shaft B1021, and the bottom of the second sliding block B1032 is movably connected with the right end of a second sliding shaft B1022; charging upper portion carries out mechanical fastening to unmanned vehicles through spacing sliding shaft, spacing sliding block, guarantees the life and the structural strength of equipment, avoids appearing the fixed problem of mistake when unmanned vehicles descends.

The advantage of the second embodiment over the first embodiment is: electricity upper portion carries out mechanical fastening to unmanned vehicles through spacing sliding shaft, spacing sliding block, guarantees the life and the structural strength of equipment, avoids appearing the fixed problem of mistake when unmanned vehicles descends.

EXAMPLE III

The present embodiment is performed on the basis of the first and second embodiments, and mainly describes the structure of the unmanned aerial vehicle control platform charging station a based on the intelligent device.

the connecting foot rest C501 comprises a connecting rod body C5011 and a fixing rod body C5012, and the bottom end of the connecting rod body C5011 is fixedly connected with the middle section of the fixing rod body C5012. When the unmanned aerial vehicle is in a flying state, two groups of connecting foot frames C501 and two groups of auxiliary foot frames C502 are folded upwards to 90 degrees, foreign matters such as electric wires and the like when the unmanned aerial vehicle flies due to the fact that suspension is avoided, when the bottom surface of the unmanned aerial vehicle stops, the two groups of connecting foot frames C501 and the two groups of auxiliary foot frames C502 are unfolded downwards to be triangular, the two groups of connecting foot frames C501 can support the unmanned aerial vehicle, when the two groups of auxiliary foot frames C502 guarantee that the bottom surface of the unmanned aerial vehicle descends and center offset occurs, the unmanned aerial vehicle cannot be directly contacted with the ground to cause damage of the unmanned aerial vehicle, when the unmanned aerial vehicle stops at the charging station A, the two groups of connecting foot frames C501 and the two groups of auxiliary foot frames C502 are unfolded downwards to be triangular, the limiting sliding blocks are tightened up in the direction of the limiting sliding shaft to limit the connecting rod body, and after connection is completed, the charging mechanism B charges the unmanned aerial vehicle through the connecting foot frames C501.

Preferably, the fixed rod body C5012 includes a rod body C5012a, two rod body clamping blocks C5012b and a center of gravity adjusting block C5012C, two rod body clamping blocks C5012b are provided, two rod body clamping blocks C5012b are provided at the left and right middle sections of the rod body C5012a, two center of gravity adjusting blocks C5012C are provided, and two center of gravity adjusting blocks C5012C are provided at the left and right ends of the rod body C5012 a. When unmanned vehicles stop, when the body of rod body contacts with the structure of charging, body of rod presss from both sides tight piece C5012B and can press from both sides tight spacing sliding block, guarantee the stability that unmanned vehicles connects, make unmanned avoidance of when charging because factor such as wind-force disconnection, cause unmanned vehicles to damage, when unmanned vehicles prepares to take off, body of rod presss from both sides tight piece C5012B and slides to body of rod both sides, release first sliding block B1031 and second sliding block B1032, it releases and is fixed with unmanned vehicles C to release first sliding block B1031 and second sliding block B1032, the foot rest component folds up 90 degrees, unmanned vehicles takes off.

Preferably, the charging station a comprises a lighting device a1, a first charging rod a2 and a second charging rod A3, the tail end of the lighting device a1 is fixedly connected with the top end of the first charging rod a2, and the rear section of the first charging rod a2 penetrates through the upper section of the second charging rod A3 and is fixedly connected therewith;

charging station A still includes first fixed cable A4, the fixed cable A5 of second, first fixed cable A4 top and the first body of rod A2 middle section fixed connection that charges, first fixed cable A4 tail end and the second body of rod A3 upper segment fixed connection that charges, the fixed cable A5 top of second and the first body of rod A2 that charges run through the second body of rod A3 part fixed connection that charges, the fixed cable A5 of second and the second body of rod A3 upper segment fixed connection that charges. The lighting device can illuminate the ground at night, when the unmanned aerial vehicle stops, the charging station A can charge the unmanned aerial vehicle through the charging mechanism B, the charging mechanism B can be additionally installed to install a street lamp or a required position meeting requirements, the problem that a common monitor cannot be installed or the utilization rate is low after installation is solved through stopping the unmanned aerial vehicle, the monitoring dead angle is eliminated, the object is multifunctional, the use cost is greatly reduced, and the monitoring and the economic benefit are improved.

Preferably, the charging station a further comprises a wireless positioning base station a6, a ground station a 7;

the wireless positioning base station A6 captures the wireless pulse signal and sends the information of the wireless pulse signal and the time point thereof to the ground station A7;

and the ground station A7 processes the wireless pulse signals and the information of the time points thereof into three-dimensional coordinate information of the unmanned aerial vehicle relative to the first base station, and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time. Unmanned vehicles get into wireless location basic station A6 scope, and wireless location label C302 receives the location radio wave that ground station A7 sent, replies wireless pulse signal, and wireless location basic station A6 catches wireless pulse signal to send wireless pulse signal and the information of time point to ground station A7, ground station A7 will wireless pulse signal and the information processing of time point become unmanned vehicles for the three-dimensional coordinate information of first basic station, and send in real time to unmanned vehicles, unmanned vehicles revises self position through three-dimensional coordinate information, accomplishes the landing. A wireless positioning tag C302 of the unmanned aerial vehicle receives positioning radio waves sent by a ground station A7 and replies a wireless pulse signal; the wireless positioning base station A6 captures the wireless pulse signal and sends the information of the wireless pulse signal and the time point thereof to the ground station A7; the ground station A7 processes the wireless pulse signals and the information of the time points of the wireless pulse signals into three-dimensional coordinate information of the unmanned aerial vehicle relative to the first base station, and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time; the unmanned aerial vehicle corrects the position of the unmanned aerial vehicle through the three-dimensional coordinate information to finish take-off, the technical problem that the positioning is inaccurate in the take-off and landing stages of the unmanned aerial vehicle is solved, and the unmanned aerial vehicle is low in cost, high in applicability, high in anti-interference capacity and accurate in positioning.

The embodiment three phases have the advantages over the embodiments one and two: the problem that a common monitor cannot be installed or a place which is not in accordance with economic benefits is low in utilization rate after installation is solved by parking the unmanned aerial vehicle, a monitoring dead angle is eliminated, the unmanned aerial vehicle is multifunctional, the use cost is greatly reduced, and the monitoring and economic benefits are improved.

The utility model also provides an operation method of the unmanned aerial vehicle control platform based on the intelligent equipment, which comprises the following steps:

s1, stopping equipment, wherein the equipment comprises a charging station A, a charging mechanism B and an unmanned aerial vehicle C, the charging mechanism B is installed at the top end of the charging station A, the unmanned aerial vehicle C is arranged above the charging mechanism B when in a stopping state, when the unmanned aerial vehicle C stops on the charging mechanism B, the charging station A transmits power to the charging mechanism B, the unmanned aerial vehicle C can supplement power through the charging mechanism B, and at the moment, a power system of the unmanned aerial vehicle C stops working;

s2, monitoring the road surface, wherein the monitoring device C6 comprises a suspension holder C601 and a camera C602, and the camera C602 is arranged at the front end of the suspension holder C601; the suspension holder C601 comprises a first suspension fixing platform C6011, a first suspension arm C6012 and a second rotation fixing platform C6013, wherein the bottom of the first suspension fixing platform C6011 is connected with the top end of the first suspension arm C6012, and the tail end of the first suspension arm C6012 is connected with the right part of the second rotation fixing platform C6013; the suspension holder C601 further comprises a second suspension arm, the tail end of the second suspension arm is fixedly connected with the camera C602, the head end of the second suspension arm is connected with the left part of the second rotary fixing table C6013, when the unmanned aerial vehicle C is in a parking state, a power system of the unmanned aerial vehicle C stops working and stops working, a monitoring device C6 is used for monitoring roads on the road surface, energy consumption and equipment loss are reduced, meanwhile, the unmanned aerial vehicle C can be used for carrying out transferring monitoring according to road sections which are blocked or have serious violation, and monitoring cost is saved;

s3, preparing for first equipment takeoff, wherein the first sliding block B1031 comprises a first clamping groove and a first connecting shaft, the first clamping groove is arranged on the inner side of the first sliding block B1031, the outer section of the first connecting shaft is arranged in the lower section of the first sliding block B1031, and the inner section of the first connecting shaft is arranged in the first sliding block B1031; the second sliding block B1032 comprises a second clamping groove and a second connecting shaft, the second clamping groove is formed in the inner side of the second sliding block B1032, the outer section of the second connecting shaft is arranged inside the lower section of the second sliding block B1032, the inner section of the second connecting shaft is arranged inside the second sliding block B1032, the first connecting shaft and the second connecting shaft are released to pop out outwards after the first sliding shaft B1021 and the second sliding shaft B1022 pop out outwards, and the first clamping groove and the second clamping groove do not limit the unmanned aerial vehicle C any more;

s4, preparing for takeoff, wherein the fixed rod body C5012 includes a rod body C5012a, rod body clamping blocks C5012B, and center of gravity adjusting blocks C5012C, two rod body clamping blocks C5012B are provided, the two rod body clamping blocks C5012B are respectively provided at the left and right of the middle section of the rod body C5012a, the two center of gravity adjusting blocks C5012C are provided, the two center of gravity adjusting blocks C5012C are respectively provided at the left and right ends of the rod body C5012a, the rod body clamping blocks C5012B slide towards the two sides of the rod body C5012a, the first sliding block B1031 and the second sliding block B1032 are released to be fixed with the unmanned aerial vehicle C, the foot rest member C5 is folded upwards by 90 degrees, and the unmanned aerial vehicle is driven by the first sliding block B1031 and the second sliding block B1032 are released;

s5, information transfer, wherein the charging station A further comprises a wireless positioning base station A6 and a ground station A7; the wireless positioning base station A6 captures the wireless pulse signal and sends the information of the wireless pulse signal and the time point thereof to the ground station A7; the signal receiver C3 comprises an alarm module C301, a wireless positioning label C302, a manual correction module C303 and a position correction module C304; the alarm module C301 alarms when the unmanned aerial vehicle deviates from a preset coordinate threshold range, and starts automatic position correction; the wireless positioning tag C302 is used for receiving positioning radio waves sent by the ground station A7 and replying wireless pulse signals; the manual correction module C303 is used for correcting the position of the unmanned aerial vehicle when the unmanned aerial vehicle loses the automatic position correction capability; the position correction module C304 corrects the position of the unmanned aerial vehicle according to the three-dimensional coordinate information; and the ground station A7 processes the wireless pulse signals and the information of the time points thereof into three-dimensional coordinate information of the unmanned aerial vehicle relative to the ground station A7, and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time. By judging the strength of the remote control signal received by the signal receiver C3, when the strength of the remote control signal received by the signal receiver C3 is lower than a set threshold value, the unmanned aerial vehicle is controlled to approach the ground station A7 according to the position information and the position information of the ground station A7, so that the unmanned aerial vehicle can be prevented from flying too far to lose control due to improper operation; furthermore, the data interruption time of the position correction module C304 is also judged, when the data transmission interruption time of the position correction module C304 exceeds the preset time, the unmanned aerial vehicle automatically returns, and when the unmanned aerial vehicle loses contact with the ground station A7, the unmanned aerial vehicle is controlled to fly to the initial takeoff position, so that safety accidents caused by the fact that the unmanned aerial vehicle loses control are prevented, and the safety of the unmanned aerial vehicle is improved;

s6, equipment is monitored in the air, the unmanned aerial vehicle C after taking off uses the monitoring device C6 to monitor and survey the air and the ground, the monitoring range is expanded, data are collected quickly, the unmanned aerial vehicle can arrive at the accident site more quickly, and after the air monitoring is finished, the unmanned aerial vehicle can be returned to an original charging station or dispatched to stop at the charging station nearby.

The foregoing is merely an example of the present invention, and common general knowledge in the field of known specific structures and characteristics is not described herein in any greater extent than that known in the art at the filing date or prior to the priority date of the application, so that those skilled in the art can now appreciate that all of the above-described techniques in this field and have the ability to apply routine experimentation before this date can be combined with one or more of the present teachings to complete and implement the present invention, and that certain typical known structures or known methods do not pose any impediments to the implementation of the present invention by those skilled in the art. It should be noted that, for those skilled in the art, without departing from the structure of the present invention, several changes and modifications can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent.

Claims

1. An unmanned aerial vehicle control platform control method based on intelligent equipment is characterized in that: the unmanned aerial vehicle control platform based on the intelligent equipment comprises a charging station (A), a charging mechanism (B) and an unmanned aerial vehicle (C), wherein the charging mechanism (B) is installed at the top end of the charging station (A), and the unmanned aerial vehicle (C) is arranged above the charging mechanism (B) in a parking state;

the charging station (A) comprises a lighting device (A1), a first charging rod body (A2) and a second charging rod body (A3), wherein the tail end of the lighting device (A1) is fixedly connected with the top end of the first charging rod body (A2), and the rear section of the first charging rod body (A2) penetrates through the upper section of the second charging rod body (A3) and is fixedly connected with the upper section of the second charging rod body;

the charging station (A) further comprises a first fixed cable (A4) and a second fixed cable (A5), the top end of the first fixed cable (A4) is fixedly connected with the middle section of the first charging rod body (A2), the tail end of the first fixed cable (A4) is fixedly connected with the upper section of the second charging rod body (A3), the top end of the second fixed cable (A5) is fixedly connected with the first charging rod body (A2) in a manner of penetrating through the part of the second charging rod body (A3), and the second fixed cable (A5) is fixedly connected with the upper section of the second charging rod body (A3);

the unmanned aerial vehicle (C) comprises a four-axis frame (C1), a machine shell (C2), a signal receiver-transmitter (C3) and a flight controller (C4), wherein the four-axis frame (C1) is fixedly connected with the machine shell (C2), the signal receiver-transmitter (C3) is installed at the top of the machine shell (C2), the flight controller (C4) is arranged in front of the signal receiver-transmitter (C3), and the bottom of the flight controller (C4) is fixedly connected with the top of the machine shell (C2);

the unmanned aerial vehicle (C) further comprises a foot stand member (C5) and a monitoring device (C6), wherein the foot stand member (C5) is installed at the bottom of the machine shell (C2), and the monitoring device (C6) is arranged at the rear section of the bottom of the machine shell (C2);

the foot rest component (C5) comprises two groups of connecting foot rests (C501) and two groups of auxiliary foot rests (C502), the two groups of connecting foot rests (C501) are respectively installed at the left end and the right end of the bottom of the machine shell (C2), and the two groups of auxiliary foot rests (C502) are installed at the rear end of the bottom of the machine shell (C2);

the connecting foot rest (C501) comprises a connecting rod body (C5011) and a fixing rod body (C5012), and the bottom end of the connecting rod body (C5011) is fixedly connected with the middle section of the fixing rod body (C5012);

the fixed rod body (C5012) comprises a rod body (C5012 a), two rod body clamping blocks (C5012 b) and two gravity center adjusting blocks (C5012C), wherein the two rod body clamping blocks (C5012 b) are respectively arranged on the left and right sides of the middle section of the rod body (C5012 a), the two gravity center adjusting blocks (C5012C) are respectively arranged on the left and right ends of the rod body (C5012 a);

the monitoring device (C6) comprises a suspension holder (C601) and a camera (C602), and the camera (C602) is arranged at the front end of the suspension holder (C601);

the suspension holder (C601) comprises a first suspension fixing platform (C6011), a first suspension arm (C6012) and a second rotation fixing platform (C6013), the bottom of the first suspension fixing platform (C6011) is connected with the top end of the first suspension arm (C6012), and the tail end of the first suspension arm (C6012) is connected with the right portion of the second rotation fixing platform (C6013);

the suspension holder (C601) further comprises a second suspension arm, the tail end of the second suspension arm is fixedly connected with the camera (C602), and the head end of the second suspension arm is connected with the left part of a second rotary fixing table (C6013);

the four-axis rack (C1) comprises a paddle (C101), a rotating shaft (C102) and a connecting shaft (C103), the paddle (C101) is mounted at the upper end of the rotating shaft (C102) and movably connected with the rotating shaft (C102), and the rotating shaft (C102) is fixedly connected with the machine shell through the connecting shaft (C103);

the signaling receiver (C3) comprises an alarm module (C301), a wireless positioning tag (C302), a manual correction module (C303) and a position correction module (C304);

the alarming module (C301) gives an alarm when the unmanned aerial vehicle deviates from a preset coordinate threshold range, and starts automatic position correction;

the wireless positioning tag (C302) receives positioning radio waves sent by the ground station and replies a wireless pulse signal;

the manual correction module (C303) corrects the position of the unmanned aerial vehicle when the unmanned aerial vehicle loses the automatic position correction capability;

the position correction module (C304) corrects the position of the unmanned aerial vehicle according to the three-dimensional coordinate information;

the charging mechanism (B) comprises a charging upper part (B1) and a charging lower part (B2), and the charging upper part (B1) is arranged above the charging lower part (B2);

the charging upper part (B1) comprises a charging seat (B101), a limiting sliding shaft (B102) and a limiting sliding block (B103), the inner section of the limiting sliding shaft (B102) is arranged inside the charging seat (B101), the outer end of the limiting sliding shaft (B102) protrudes out of the side part of the charging seat (B101), and the limiting sliding shaft (B102) is connected with the limiting sliding block (B103);

the limiting sliding shaft (B102) comprises a first sliding shaft (B1021) and a second sliding shaft (B1022), the first sliding shaft (B1021) is arranged at the right section inside the charging seat (B101), and the second sliding shaft (B1022) is arranged at the left section inside the charging seat (B101);

the limit sliding block (B103) comprises a first sliding block (B1031) and a second sliding block (B1032), the bottom of the first sliding block (B1031) is movably connected with the left end of a first sliding shaft (B1021), and the bottom of the second sliding block (B1032) is movably connected with the right end of a second sliding shaft (B1022);

the specific control method is as follows,

s1, stopping equipment, wherein the equipment comprises a charging station (A), a charging mechanism (B) and an unmanned aerial vehicle (C), the charging mechanism (B) is installed at the top end of the charging station (A), the unmanned aerial vehicle (C) is arranged above the charging mechanism (B) in a stopping state, when the unmanned aerial vehicle (C) stops at the charging mechanism (B), the charging station (A) transmits electric power to the charging mechanism (B), the unmanned aerial vehicle (C) can supplement the power through the charging mechanism (B), and at the moment, a power system of the unmanned aerial vehicle (C) stops working;

s2, monitoring the road surface, wherein the monitoring device (C6) comprises a suspension holder (C601) and a camera (C602), and the camera (C602) is arranged at the front end of the suspension holder (C601); the suspension holder (C601) comprises a first suspension fixing platform (C6011), a first suspension arm (C6012) and a second rotation fixing platform (C6013), the bottom of the first suspension fixing platform (C6011) is connected with the top end of the first suspension arm (C6012), and the tail end of the first suspension arm (C6012) is connected with the right portion of the second rotation fixing platform (C6013); the suspension holder (C601) further comprises a second suspension arm, the tail end of the second suspension arm is fixedly connected with the camera (C602), the head end of the second suspension arm is connected with the left part of the second rotary fixing table (C6013), when the unmanned aerial vehicle (C) stops, a power system of the unmanned aerial vehicle (C) stops working, and a monitoring device (C6) is used for road monitoring on a road surface;

s3, preparing for first equipment takeoff, wherein the first sliding block (B1031) comprises a first clamping groove and a first connecting shaft, the first clamping groove is arranged on the inner side of the first sliding block (B1031), the outer section of the first connecting shaft is arranged in the lower section of the first sliding block (B1031), and the inner section of the first connecting shaft is arranged in the first sliding block (B1031); the second sliding block (B1032) comprises a second clamping groove and a second connecting shaft, the second clamping groove is formed in the inner side of the second sliding block (B1032), the outer section of the second connecting shaft is arranged in the lower section of the second sliding block (B1032), the inner section of the second connecting shaft is arranged in the second sliding block (B1032), the first connecting shaft and the second connecting shaft are released to be outwards popped out after the first sliding shaft (B1021) and the second sliding shaft (B1022) are outwards popped out, and the first clamping groove and the second clamping groove do not limit the unmanned aerial vehicle (C);

s4, preparing a second device for takeoff, where the fixed rod body (C5012) includes a rod body (C5012 a), rod body clamping blocks (C5012B), and center of gravity adjusting blocks (C5012C), two rod body clamping blocks (C5012B) are provided, the two rod body clamping blocks (C5012B) are respectively provided at the left and right sides of the middle section of the rod body (C5012 a), two center of gravity adjusting blocks (C5012C) are provided, the two center of gravity adjusting blocks (C5012C) are respectively provided at the left and right ends of the rod body (C5012 a), the rod body clamping block (C5012B) slides to the two sides of the rod body (C5012 a), the first sliding block (B1031) and the second sliding block (B1032) are released to be fixed to the unmanned aerial vehicle (C), and the foot stool member (C5) is folded upwards by 90 degrees;

s5, information transfer, wherein the charging station (A) further comprises a wireless positioning base station (A6) and a ground station (A7); the wireless positioning base station (A6) captures the wireless pulse signal and sends the wireless pulse signal and the information of the time point thereof to the ground station; the signaling receiver (C3) comprises an alarm module (C301), a wireless positioning label (C302), a manual correction module (C303) and a position correction module (C304); the alarming module (C301) gives an alarm when the unmanned aerial vehicle deviates from a preset coordinate threshold range, and starts automatic position correction; a wireless positioning tag (C302) which receives positioning radio waves sent by the ground station and replies wireless pulse signals; a manual correction module (C303) which corrects the position of the unmanned aerial vehicle when the unmanned aerial vehicle loses the automatic position correction capability; a position correction module (C304) for correcting the position of the unmanned aerial vehicle according to the three-dimensional coordinate information; the ground station (A7) processes the wireless pulse signals and the information of the time points thereof into three-dimensional coordinate information of the unmanned aerial vehicle relative to the ground station (A7), and sends the three-dimensional coordinate information to the unmanned aerial vehicle in real time, the strength of the remote control signals received by the signal transceiver (C3) is judged, and when the strength of the remote control signals received by the signal transceiver (C3) is lower than a set threshold value, the unmanned aerial vehicle is controlled to approach the ground station (A7) according to the position information of the ground station (A7), so that the unmanned aerial vehicle can be prevented from flying too far and losing control due to improper operation; further, the data interruption time of the position correction module (C304) is also judged, when the data transmission interruption of the position correction module (C304) exceeds the preset time, the unmanned aerial vehicle automatically returns, and when the unmanned aerial vehicle is out of contact with the ground station (A7), the unmanned aerial vehicle is controlled to fly to the initial takeoff position;

s6, equipment is monitored in the air, the unmanned aerial vehicle (C) after taking off uses the monitoring device (C6) to monitor and survey the air and the ground, the monitoring range is expanded, data are collected quickly, the unmanned aerial vehicle can arrive at the incident place more quickly, and after the air monitoring is finished, the unmanned aerial vehicle can be returned to an original charging station or dispatched to stop at the charging station nearby.