CN109491408A - A kind of unmanned plane can be used for doors structure detection - Google Patents

A kind of unmanned plane can be used for doors structure detection Download PDF

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Publication number
CN109491408A
CN109491408A CN201811421191.3A CN201811421191A CN109491408A CN 109491408 A CN109491408 A CN 109491408A CN 201811421191 A CN201811421191 A CN 201811421191A CN 109491408 A CN109491408 A CN 109491408A
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data
module
aerial vehicle
unmanned aerial
unmanned plane
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冯正坤
苏毅
卢卓成
崔澜潇
刘国懿
陈祥
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Nanjing Forestry University
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Nanjing Forestry University
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Priority to CN201811421191.3A priority Critical patent/CN109491408A/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/02Measuring arrangements characterised by the use of optical techniques for measuring length, width or thickness
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C11/00Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
    • G01C11/04Interpretation of pictures
    • G01C11/06Interpretation of pictures by comparison of two or more pictures of the same area
    • G01C11/08Interpretation of pictures by comparison of two or more pictures of the same area the pictures not being supported in the same relative position as when they were taken
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/12Target-seeking control

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Multimedia (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Investigating Materials By The Use Of Optical Means Adapted For Particular Applications (AREA)

Abstract

本发明公开了一种可用于室内结构检测的无人机,属于结构检测技术领域,用于解决替代专业工程人员进入危险房屋室内检测的问题。其包括无人机主体、地面控制站、数据处理中心和无人机上设置的搭载模块组合四部分,搭载模块组合包括图像采集模块、传感器组、飞行状态处理器、通信模块和存储模块。地面控制站包括遥控器与显示屏。数据处理中心可从拍摄得到的图像中获取裂缝的尺寸数据。本发明巧妙地利用无人机拍摄的图像,用数据处理中心对室内结构构件进行裂缝长度和宽度的量测,快速判断房屋的健康状态,给出房屋结构的初步鉴定结论,操作简单,数据处理速度快,数据可靠性高。

The invention discloses an unmanned aerial vehicle which can be used for indoor structure detection, belongs to the technical field of structure detection, and is used for solving the problem of replacing professional engineers to enter dangerous houses for indoor detection. It includes four parts: the main body of the drone, the ground control station, the data processing center, and the combination of mounted modules set on the drone. The combination of mounted modules includes an image acquisition module, a sensor group, a flight status processor, a communication module, and a storage module. The ground control station includes a remote control and a display. The data processing center can obtain the size data of the cracks from the captured images. The invention cleverly utilizes the images captured by the unmanned aerial vehicle, uses the data processing center to measure the crack length and width of the indoor structural components, quickly judges the health state of the house, and gives the preliminary appraisal conclusion of the house structure, with simple operation and data processing. Fast speed and high data reliability.

Description

A kind of unmanned plane can be used for doors structure detection
Technical field
The present invention relates to a kind of unmanned plane that can be used for doors structure detection, especially one kind can be used for indoor flaw size The unmanned plane of measure analysis.
Background technique
Modern architecture is in its normal use process or after undergoing the natural calamities such as earthquake, due to construction material self reason And imposed load influences, structure can be deformed, differential settlement, it is serious destroy etc. unfavorable phenomenon cause structural instability or Lose bearing capacity.Although most of building structure is all work with cracking in Practical Project, when fracture width is more than threshold Architectural appearance is not only influenced when value, is given user's feeling of risk, seriously also be will affect bearing capacity, the durability of component.
Crack Detection looks for and measures to split engineering by professional testing staff with fracture detecting instrument or scale in practice Stitch size.But the problems such as this traditional detection method has at high cost, low efficiency, manpower safety guarantee is low, precision is low, especially After earthquake, aftershock may continue long period of time, and aftershock earthquake magnitude also it is difficult to predict, allow at this time staff into Enter to carry out operation inside house that larger threat is had to its personal safety.It is replaced in contrast using the unmanned plane of small size artificial Detected, in the way of the unique Fast Labeling of unmanned plane itself and visual angle advantage, it can be achieved that multi-angle, all standing bat It takes the photograph, detection data data can be made more complete;Possess numerous advantages such as feature easy to operate, at low cost, it is often more important that can be with Reduce the risk of staff.
Existing patent mainly solves the problems, such as that unmanned plane carries out whole detection to building or road, river in outdoor, But lack the unmanned plane for being able to enter and carrying out thin portion detection inside structure space.For example, patent CN201720977296 is proposed A kind of engineering construction Crack Detection unmanned plane, which can realize the detection of the width to building surface crack, but not solve Certainly the positioning for the unmanned plane for enabling to office work and to component to be measured carry out pin numbers the problems such as.In addition earthquake disaster In dilapidated house detection after evil, due to that may meet with aftershock at any time, it is extremely hazardous that testing staff, which enters the room and carries out thin portion detection, 's.Therefore, the miniaturization unmanned plane that indoor detection function is added is necessary the dilapidated house detection of similar situation.
Summary of the invention
In order to solve the above-mentioned technical problem, the present invention proposes a kind of unmanned plane that can be used for doors structure detection, for solving Certainly lack the problem of can entering the room the miniaturization unmanned plane detected to structural detail instantly.Concrete composition skill of the invention Art scheme are as follows: can be used for the unmanned plane of doors structure detection, including at unmanned plane main body, corresponding ground control station, ground data The carrying block combiner being arranged on reason center and unmanned plane.
Image capture module, sensing are arranged on the carrying composite module for the carrying block combiner being arranged in unmanned plane main body Device group, state of flight processor, communication module and memory module.Wherein, image capture module includes being divided into key data acquisition Module and auxiliary shooting module, for acquiring the image data for facilitating building structure safety detection, and pass through communication module Collected data are transferred to central station, carry out Data Post, are detected with obtaining for safety of structure Index data.The sensor group on composite module is carried, for acquiring Flight Condition Data, and is transmitted to flight shape State processor makes it make the instruction of flight attitude according to the actual situation.The state of flight processor on composite module is carried, is used In the Flight Condition Data that the transmission of receiving sensor group comes, unmanned plane during flying state and position are adjusted according to a pre-set procedure It sets, after the image data received and status data pretreatment, is transferred to communication module, then described image data are saved in Memory module.Such as in flight course, in order to hide structural obstructions object manipulation unmanned plane using a variety of flight attitudes close to shooting Point adjusts the verticality etc. of unmanned plane when reaching camera site.Wherein, communication module is used for reception state data and picture number According to, and status data and image data are transferred to ground control station, memory module be used to store the status data that receives with Image data.
Image capture module, communication module, coprocessor in the combination respectively with ground control centre and data processing Center is connected by wireless signal, and the exchange of data can be carried out between them, and control signal can be sent by ground control station It is received again by unmanned plane, image data, Flight Condition Data etc. can also be transmitted to ground control station sum number by communication module According to processing center.
Key data acquisition module included by image capture module is used for the acquisition of image information.The module by focal length, Two groups of camera compositions of short focus, work respectively.When carrying out Image Acquisition, the same time is only by wherein one piece of camera lens work Make.In use, usage scenario is judged by operator, for example, carrying out length direction when needing to carry out the biggish crack of length When measurement, or when needing detection structure beyond the region of objective existence contour line, telephoto lens is called to carry out Image Acquisition by operator;When need When badly being detected to thin portion breakage, such as when needing to measure the width in crack, then by operator call short-focus lens into Row shooting.Two groups of cameras are operated respectively by ground control station, independent to transmit data to the ground, are not interfere with each other, have been widened image and adopted The scope of application of collection.
The image capture module except as focal length, in addition to key data acquisition module composed by short focus camera, further include Corresponding auxiliary shooting module and lighting module.Assisting shooting module includes infrared camera, and infrared camera is connected with ground control station, Control station and data processing centre send data and receive the control instruction of ground control station transmission to the ground.The module is for working as Key data acquisition module under dim light or no light conditions can not normal use when to structural body carry out image information acquisition, Such as the module can be used to work inside the house to topple, in the spaces such as basement.
The lighting module of unmanned plane setting carries out remote control operation by the connection with ground control station.Lighting module For being illuminated under low light environment or no light conditions so that unmanned plane in this case can with normal flight and work, and Under low light environment or no light condition, light filling is carried out, makes unmanned plane that can shoot to obtain clearly image data.The lighting module It is made of four pieces of LED lamp beads, the light and shade of light can be adjusted according to the number that lamp bead is lighted, the photo for preventing shooting from obtaining occurs Overexposure.
Sensor group is used to be monitored and controlled the state of flight of unmanned plane.The sensor group is sensed by high-precision laser range-finding Device, obliquity sensor, acceleration transducer and ambient light sensor composition, and handled by wired connection to the state of flight Device sends data.Wherein, high-precision laser range-finding sensor is for acquiring range data, for judging unmanned plane space indoors Relative position, two one group, totally six groups, be arranged on the front, back, left, right, up, down six direction of unmanned plane, work Mode are as follows: first determine a plane to be measured, emit distance measuring laser beams from upfront sensor to metope, compare the length of twice laser beam Degree, is finely adjusted, until the length of twice light beam is identical;Subsequent other five groups of sensors are repeated in this operation, finally make Unmanned plane and indoor six planes keep Relative vertical, reduce shooting angle bring pattern distortion with this.Obliquity sensor is adopted Collect flight attitude data, including unmanned plane rotor inclination angle and image capture module inclination angle, it is outstanding to be used to matching program setting unmanned plane The angle in stopping time and horizontal plane guarantees that the angle of the unmanned plane after determining position will not deviate.Acceleration transducer cooperation Range sensor uses, and for acquiring aircraft course line number evidence, prevents unmanned plane from colliding with works.Obliquity sensor The course of work with acceleration transducer be it is known, details are not described herein.Ambient light sensor is for acquiring ambient light conditions Data to monitor the light condition under detection environment, can matching program realize and remind switching of the operator to camera, if environment Light intensity is less than definite value, then reminds user to call infrared camera according to field condition or lighting module is called to carry out light filling.
The communication module and data memory module for the carrying block combiner being arranged on unmanned plane, for image capture module Data collected are transmitted and are saved, while guaranteeing the stabilization data connection between ground control station and unmanned plane.Communication Module is connected using Wi-Fi signal with ground control station.Data memory module provides multiple interfaces, and it is outer to can access storage card etc. Connect storage equipment.
The state of flight processor for the carrying block combiner being arranged on unmanned plane.The processor is mainly to the flight of unmanned plane Status data is handled.The collected data of image capture module and sensor group institute, including image data, apart from number According to, attitude data, course data and light condition data, handled by the processor, to guarantee its timeliness.Meanwhile The processor can pre-process institute's acquired image data, i.e., be numbered, be grouped, sort out to image data, improve The working efficiency of central station.
Complete equipment includes ground control station, which includes remote controler and user terminal display screen, is furnished with mating operation Software.Earth station can real-time display unmanned plane various posture informations and measurement camera obtain high quality image information, be used for The state of flight of unmanned plane is controlled and adjusted, and is operated by operator.
Central station possesses independent operational capability, handles data using high-performance computer, operation is independent Application program receives the collected data of unmanned plane institute by wireless transmission or carrier transmission, and carries out to the data received Analysis processing, mainly differentiates the edge in crack, then carries out the measurement of size.
The present invention provides a kind of unmanned planes that can be used for doors structure detection.Have it is following the utility model has the advantages that
When unmanned plane carries out operation, the collaborative work of preposition range sensor group, Automatic-searching and the first face can be passed through The position of wall body vertical.It is adjusted by gyroscope, keeps unmanned plane spiral pushing aid axis and range laser line institute vertical at face, And dimensional Cartesian coordinates system is established as origin, surveyed component is determined by the relative coordinate of unmanned plane in space Position.The distortion that the image that shooting obtains occurs can be effectively reduced after the completion of positioning.When detection, unmanned plane is suitable in the direction of the clock Secondary rotation calls focal length camera to be successively integrally scanned to metope.At the same time, it can be completed by central station Number work to the room and other corresponding walls, and establish corresponding file respectively to store correspondence image information. After the completion of the detection in big face, operator Selection and call short focus camera then can further examine thin portion as needed It surveys.Cooperate ambient light sensor, operator can be assisted to judge whether to need to call auxiliary shooting module or lighting module to dark Portion carries out data acquisition.Lighting module can carry out brightness regulation by ground control station by operator.Acceleration transducer can So that unmanned plane has the function of intelligent anticollision.Gained image data is transmitted to central station by communication module, Processing obtains specific size data, comprising: the length dimension in crack, the width dimensions in crack, house length, width and height three-dimensional dimension, knot Structure and vertical line degrees of offset.After obtaining above-mentioned data, further according to the threshold value of setting, building safety conclusion, including knot are obtained The bearing capacity of structure and the reliability of normal use.The unmanned machine equipment that the present invention is reached has applied widely, small-sized Change, light-weighted advantage.
Detailed description of the invention
It in order to more clearly illustrate the technical solutions in the embodiments of the present invention, below will be in embodiment technical description Required attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only some realities of the invention Example is applied, it for those of ordinary skill in the art, without creative efforts, can also be according to these attached drawings Obtain other attached drawings.
Fig. 1 is that unmanned plane each section forms stratal diagram;
Fig. 2 is unmanned plane each section correlation figure;
Fig. 3 is unmanned plane work flow diagram.
In FIG. 1 to FIG. 3, included part is listed below: 1 unmanned plane main body;2 ground control stations;3 Data processings The heart;4 block combiners;5 image capture modules;6 sensor groups;7 state of flight processors;8 communication modules;9 memory modules;10 is main Want data acquisition module;11 auxiliary shooting modules;12 focal length cameras;13 short focus cameras;14 high-precision laser range-finding sensors;15 Obliquity sensor;16 acceleration transducers;17 ambient light sensors;18 lighting modules;19 remote controlers;20 display screens;21 is infrared Camera.
Specific embodiment
For it is a kind of can be used for doors structure detection unmanned plane comprising unmanned plane main body, corresponding ground control station and Central station.Wherein, block combiner is carried in setting on unmanned plane.Ground control station includes instruction issue remote controler And display screen.
The composition of unmanned plane equipment components, connection relationship are as follows: laser range sensor is with 12 pieces, two one group, altogether It six groups, is arranged on the front, back, left, right, up, down six direction of unmanned plane.Image capture module is integrated in gondola, Using stacked layout, from the top down successively are as follows: key data acquisition module, auxiliary data acquisition module, lighting module.Environment Optical sensor and auxiliary data acquisition module integrate.Obliquity sensor, acceleration transducer and gyroscope are placed in nobody At machine inside center.The sensor passes through bus and is connected with state of flight processor, state of flight processor and transmission Module is connected, and image capture module is connected with transmission module with memory module simultaneously.The above element passes through communication module With in earth station ground control station and central station be connected.State of flight processor, transmission module, storage mould Block, communication module, obliquity sensor, acceleration transducer and gyroscope are integrated in aircraft interior.
It needs first to manually control unmanned plane before use to fly from outdoor large space to indoor pre-position, and is arranged corresponding Detection task, unmanned plane completes to System self-test after being powered, connects unmanned plane and earth station equipment, carry out real-time synchronization biography It is defeated, it can start to carry out coordinate measuring automatically and calculate, and corresponding file to be measured is added to designated position, fulfil assignment Preceding initial setting.
Concrete operating principle and the course of work of the present invention are as follows: the first step, detection prepare.First by the operation of ground control station Personnel accordingly control program by unmanned plane and assign command adapted thereto to unmanned plane, and control unmanned plane flies to test point to be measured.Into The debugging of row relevant parameter, parameter specifically include: the selection of working face, flight time control, setting required precision, setting movement speed Degree adjusts camera parameter.After the completion of to be regulated, it is connected to the power supply of unmanned machine testing mould group, be switched on waiting system self-test.System is certainly After the completion of inspection, activate indoor positioning correlation module and its accordingly meet the tendency of line program.Second step, detection.Before being passed through by unmanned plane The collaborative work for the dual range sensor set, the position of Automatic-searching and the first face wall body vertical.Gyroscope is adjusted, is made Unmanned plane spiral pushing aid axis and range laser line institute are vertical at face, and establish dimensional Cartesian coordinates system as origin, lead to The relative coordinate of unmanned plane in space is crossed to determine the position of surveyed component.Start to detect after positioning.It hangs on this basis Stop, sequentially rotate in the direction of the clock, focal length camera is called successively to be scanned to metope, at the same time by ground data The number work to the room and other corresponding walls is completed at reason center, and establishes corresponding file respectively to store correspondence Image information.After the completion of the detection in big face, short focus camera is called then to carry out to thin portion on demand by operator further Detection.Thin portion detection specifically includes: frame structural beam, column, node, shear wall, wall between windows, staircase etc..When detection, by nothing The image capture module of man-machine upper carrying acquires the image data in the face.A room is detected in this order, after the completion Then enter Next Room, repeats identical operation.It is then the end of one-time detection after whole predetermined detection target to be done.The Three steps, analyze data.After the image data of unmanned plane acquisition reaches central station, run by computer only Vertical application software analyzes data, and content collected includes: the length dimension in crack, the width dimensions in crack, room Room length, width and height three-dimensional dimension, structure and vertical line degrees of offset.After obtaining above-mentioned data, further according to the threshold value of setting, room is obtained Room Safety Conclusions, the reliability of bearing capacity and normal use including structure.

Claims (9)

1.一种可用于室内结构检测的无人机,其特征在于:包括无人机主体(1)、对应地面控制站(2)、地面数据处理中心(3)以及无人机上设置的搭载模块组合(4),搭载模块组合(4)上设置图像采集模块(5)、传感器组(6)、飞行状态处理器(7)、通信模块(8)和存储模块(9);1. an unmanned aerial vehicle that can be used for indoor structure detection, it is characterized in that: comprise unmanned aerial vehicle main body (1), corresponding ground control station (2), ground data processing center (3) and the carrying module that is set on the unmanned aerial vehicle The combination (4), an image acquisition module (5), a sensor group (6), a flight state processor (7), a communication module (8) and a storage module (9) are arranged on the carrying module combination (4); 其中:图像采集模块(5)包括分为主要数据采集模块(10)与辅助拍摄模块(11),用于采集图像数据,并将采集到的数据传输到地面数据处理中心(3);传感器组(6),用于采集飞行状态数据进行对无人机的调整;飞行状态处理器(7),用于接收传感器组(6)传输来的飞行状态数据,根据预先设定的程序调整无人机飞行状态与位置,将接收到的图像数据和状态数据预处理后传输到通信模块(8),再将所述图像数据保存到存储模块(9);通信模块(8)用于接收状态数据和图像数据,并将状态数据和图像数据传输到地面控制站(2);存储模块(9)用于存储接收到的状态数据和图像数据。Wherein: the image acquisition module (5) includes a main data acquisition module (10) and an auxiliary shooting module (11) for acquiring image data and transmitting the acquired data to a ground data processing center (3); a sensor group (6), used to collect the flight state data to adjust the UAV; the flight state processor (7) is used to receive the flight state data transmitted from the sensor group (6), and adjust the unmanned aerial vehicle according to the preset program The flight status and position of the aircraft are preprocessed, and the received image data and status data are preprocessed and transmitted to the communication module (8), and then the image data is stored in the storage module (9); the communication module (8) is used for receiving status data and image data, and transmit the state data and image data to the ground control station (2); the storage module (9) is used for storing the received state data and image data. 2.根据权利要求1所述的可用于室内结构检测无人机,其特征在于:所述图像采集模块(5)的主要数据采集模块(10)包括高分辨率长焦摄像机(12)和短焦相机(13),高分辨率长焦摄像机(12)和短焦相机(13)彼此独立,分别向地面传输数据。两种相机可通过地面控制站(2)分别控制,方便用户根据具体操作需求进行自由切换。2. The unmanned aerial vehicle that can be used for indoor structure detection according to claim 1 is characterized in that: the main data acquisition module (10) of the image acquisition module (5) comprises a high-resolution telephoto camera (12) and a short A focus camera (13), a high-resolution telephoto camera (12) and a short focus camera (13) are independent of each other and transmit data to the ground respectively. The two cameras can be controlled separately by the ground control station (2), which is convenient for users to switch freely according to specific operation requirements. 3.根据权利要求1所述的可用于室内结构检测无人机,其特征在于:所述图像采集模块(5)的辅助拍摄模块(11)包括红外相机(21),红外相机(21)通过通信模块(8)与地面数据处理中心(3)连接。3. The unmanned aerial vehicle that can be used for indoor structure detection according to claim 1, characterized in that: the auxiliary shooting module (11) of the image acquisition module (5) comprises an infrared camera (21), and the infrared camera (21) passes through the The communication module (8) is connected with the ground data processing center (3). 4.根据权利要求1所述的可用于室内结构检测无人机,其特征在于:所述传感器组(6)用于监测控制无人机的飞行状态,包括高精度激光测距传感器(14)、倾角传感器(15)、加速度传感器(16)和环境光传感器(17),高精度激光测距传感器(14)、倾角传感器(15)、加速度传感器(16)和环境光传感器(17)均通过有线连接向所述飞行状态处理器(7)发送数据。4. The drone that can be used for indoor structure detection according to claim 1, wherein the sensor group (6) is used to monitor and control the flying state of the drone, including a high-precision laser ranging sensor (14) , tilt sensor (15), acceleration sensor (16) and ambient light sensor (17), high-precision laser ranging sensor (14), tilt sensor (15), acceleration sensor (16) and ambient light sensor (17) all pass The wired connection sends data to the flight state processor (7). 5.根据权利要求1所述的可用于室内结构检测无人机,其特征在于:所述通信模块(8)为无线传输模块。5 . The unmanned aerial vehicle according to claim 1 , wherein the communication module ( 8 ) is a wireless transmission module. 6 . 6.根据权利要求1所述的可用于室内结构检测无人机,其特征在于:设置照明模块(18),通过与地面控制站(2)的连接远程控制操作,照明模块(18)用于对较暗处进行照明。6. The unmanned aerial vehicle that can be used for indoor structure detection according to claim 1 is characterized in that: a lighting module (18) is provided, and the remote control operation through the connection with the ground control station (2), the lighting module (18) is used for Illuminate darker places. 7.根据权利要求1所述的可用于室内结构检测无人机,其特征在于:所述飞行状态处理器(7)用于接收并处理无人机飞行状态数据。通过图像采集模块(5)、传感器组(6)、飞行状态处理器(7)的组合工作,使无人机具备在室内自动定位并采集坐标数据的能力。7. The UAV for indoor structure detection according to claim 1, wherein the flight state processor (7) is used for receiving and processing UAV flight state data. Through the combined work of the image acquisition module (5), the sensor group (6) and the flight state processor (7), the UAV has the ability to automatically locate and collect coordinate data indoors. 8.根据权利要求1所述的可用于室内结构检测的无人机,其特征在于:地面控制站包括遥控器(19)和显示屏(20),集成了对无人机的飞行控制以及指令发射功能,控制人员在做出指令后可由地面控制站(2)发送至无人机接收器,对无人机的飞行状态进行人工调节与修正。8. The drone that can be used for indoor structure detection according to claim 1, wherein the ground control station comprises a remote controller (19) and a display screen (20), which integrates flight control and instructions to the drone With the launch function, the controller can send the command from the ground control station (2) to the UAV receiver to manually adjust and correct the flight state of the UAV. 9.根据权利要求1所述的可用于室内结构检测的无人机,其特征在于:数据处理中心(3)用于对接收到的数据进行处理,可进行图像数据的分类、编号,以及后期识别处理,可以统筹处理无人机的飞行状态数据。9. The unmanned aerial vehicle that can be used for indoor structure detection according to claim 1 is characterized in that: the data processing center (3) is used to process the received data, and can carry out classification, numbering of image data, and post-processing. Recognition processing can coordinate the processing of the flight status data of the UAV.
CN201811421191.3A 2018-11-22 2018-11-22 A kind of unmanned plane can be used for doors structure detection Pending CN109491408A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109974585A (en) * 2019-04-18 2019-07-05 甘肃博程技术咨询服务有限公司 A kind of elevator shaft structure recognition and data measurement unit
CN110161515A (en) * 2019-04-23 2019-08-23 武昌理工学院 A House Measurement System Based on Laser Distance Measurement
CN111103297A (en) * 2020-01-20 2020-05-05 无锡市建筑工程质量检测中心 Non-contact detection method and system for quality of building outer wall surface
CN111103296A (en) * 2020-01-20 2020-05-05 无锡市建筑工程质量检测中心 A data measurement control processing device of a non-contact detection system for the quality of building exterior wall layers
CN112130167A (en) * 2020-07-03 2020-12-25 北京中电科卫星导航系统有限公司 Mobile millimeter wave human body security inspection system
CN112378336A (en) * 2020-11-13 2021-02-19 南通中远海运川崎船舶工程有限公司 Cabin capacity measuring system based on unmanned aerial vehicle and measuring method thereof
CN118090742A (en) * 2024-04-18 2024-05-28 江西赣粤高速公路股份有限公司 Image acquisition method for detecting hinge joint damage of prefabricated bridge

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109974585A (en) * 2019-04-18 2019-07-05 甘肃博程技术咨询服务有限公司 A kind of elevator shaft structure recognition and data measurement unit
CN110161515A (en) * 2019-04-23 2019-08-23 武昌理工学院 A House Measurement System Based on Laser Distance Measurement
CN111103297A (en) * 2020-01-20 2020-05-05 无锡市建筑工程质量检测中心 Non-contact detection method and system for quality of building outer wall surface
CN111103296A (en) * 2020-01-20 2020-05-05 无锡市建筑工程质量检测中心 A data measurement control processing device of a non-contact detection system for the quality of building exterior wall layers
CN111103297B (en) * 2020-01-20 2024-07-12 无锡市建筑工程质量检测中心 Non-contact detection method and detection system for quality of building exterior wall surface layer
CN111103296B (en) * 2020-01-20 2024-10-18 无锡市建筑工程质量检测中心 A data measurement control processing device for a non-contact detection system of building exterior wall surface quality
CN112130167A (en) * 2020-07-03 2020-12-25 北京中电科卫星导航系统有限公司 Mobile millimeter wave human body security inspection system
CN112378336A (en) * 2020-11-13 2021-02-19 南通中远海运川崎船舶工程有限公司 Cabin capacity measuring system based on unmanned aerial vehicle and measuring method thereof
CN112378336B (en) * 2020-11-13 2023-02-17 南通中远海运川崎船舶工程有限公司 Cabin capacity measuring system based on unmanned aerial vehicle and measuring method thereof
CN118090742A (en) * 2024-04-18 2024-05-28 江西赣粤高速公路股份有限公司 Image acquisition method for detecting hinge joint damage of prefabricated bridge

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