WO2013032078A1 - Method and system for unmanned airborne collection and transmission of information - Google Patents

Method and system for unmanned airborne collection and transmission of information Download PDF

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Publication number
WO2013032078A1
WO2013032078A1 PCT/KR2012/001232 KR2012001232W WO2013032078A1 WO 2013032078 A1 WO2013032078 A1 WO 2013032078A1 KR 2012001232 W KR2012001232 W KR 2012001232W WO 2013032078 A1 WO2013032078 A1 WO 2013032078A1
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WIPO (PCT)
Prior art keywords
information
air
collection
floating
collecting
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PCT/KR2012/001232
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French (fr)
Korean (ko)
Inventor
김준규
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Kim Jun-Kyu
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Publication of WO2013032078A1 publication Critical patent/WO2013032078A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/35UAVs specially adapted for particular uses or applications for science, e.g. meteorology

Definitions

  • the present invention forms a triangular point by fastening a plurality of air collection drive in a semi-convex sphere of a predetermined angle, each air collection drive is formed with a plurality of cylindrical fans connected to the rotating body based on the intermediate drive rotation point
  • each air collection drive is formed with a plurality of cylindrical fans connected to the rotating body based on the intermediate drive rotation point
  • the main body which is connected to the air collection propulsion unit and consists of each information collecting sensor, has a 3-axis gyroscope sensor, a temperature / humidity sensor, an altitude sensor, a wind speed measuring unit, and a processing unit for converting a predetermined value into information using the same; It is composed of a storage recorder for storing and recording in the form and a transmission unit for transmitting weather information to the receiver to collect weather information located on the ground, so that the control and adjustment that can be restored to the starting point of the main body.
  • the lifting fan is closed to create an air-conical cone to create a buoyancy to maintain the speed of falling down based on the buoyancy, and more Combines a large number of air collection props based on the center point for greater buoyancy and cover the case on the top to create a larger buoyancy to float in the air.
  • the rotation speed of the rotating body of the air collection propeller is controlled and controlled by the control processor for fixing, moving or turning in the place where information is collected.
  • Input information from these paths and locations is transmitted from an external processing receiver, and a processing unit is set up to automatically return to the starting point after all processing is completed.
  • UAVs unmanned aerial vehicles
  • the flight of the unmanned aerial vehicle includes an inertial navigation system for navigation equipment, a speedometer, an altimeter, and attitude control, and a GPS (Global Positioning System) for route guidance.
  • GPS Global Positioning System
  • the inertial navigation system consists of a gyroscope and an accelerometer called an inertial sensor, and measures the rotational angular velocity and linear acceleration of the unmanned aerial vehicle, and provides information on the current position, speed, altitude, azimuth, and flight attitude of the unmanned aerial vehicle.
  • an inertial sensor measures the rotational angular velocity and linear acceleration of the unmanned aerial vehicle, and provides information on the current position, speed, altitude, azimuth, and flight attitude of the unmanned aerial vehicle.
  • FLYING BODY of 1020100113141 (20101020), which is openly applied, is an upper blower composed of a rotating impeller that pumps air in an axial flow direction.
  • the upper blower is composed of a skirt-shaped fixed blade in which the upper blower is concentrically arranged. It is not the principle of the method of applying the buoyancy of the device which is lowered to the device to obtain the thrust by switching the power, and the flight control system and control method of the unmanned aerial vehicle of the disclosed 1020100016915 (20100216)
  • the vehicle can recognize the failure caused by the navigation equipment, the speedometer, and the altimeter, and excludes the current position, flight posture, azimuth, speed, and altitude measured by the navigation equipment, the speedometer, and the altimeter where the failure has occurred.
  • Flight control device of unmanned aerial vehicle capable of selectively inputting current position, flight attitude, azimuth, speed, and altitude
  • Fixed-wing method for controlling a vehicle of the way floating by on the speedometer such as the control method between the speed control and other devices, such as for keeping the lift for the aircraft as a control method for unmanned aircraft flying to the control method is not.
  • a long flight time is ensured by floating in the air by using a plurality of air collecting propulsion bodies that can continuously perform the operation of raising or lowering the altitude above a predetermined path and location, and the body itself Auto-reversible function
  • the main body rises through the triangular-shaped air collection propulsion unit so that lift force is generated for the main body floating in the air to maintain the constant altitude up to a certain altitude, and at the same time stops the rotating body according to the altitude.
  • Lifting fan is converted to the angle to collect the air, and the air collection cap and air collection case by the body is free buoyancy is formed floating even when free fall.
  • the control processing unit can adjust the rotation speed of the rotating body for each air collection propulsion unit, and the control processing unit has a communication unit that can transmit and receive with the outside.
  • the lower part has a buffer support so that the main body can take off and land regardless of the terrain.
  • the control processing unit is modularized to be used in accordance with the intended use (unmanned reconnaissance, weather measurement, communication relay, etc.) to be combined and used for each purpose.
  • an information collecting processor for transmitting initial setting information to the control processor so as to arbitrarily adjust the usage method in real time from the outside, and receiving, displaying, processing, and storing the collected information transmitted from the control processor.
  • a sensor that checks the equilibrium state of the rotating propulsion fluid at all times by constructing a convex parachute structure that connects a large number of air collection propellers to a triangular center point that can raise the body in a balanced manner and form buoyancy when descending
  • the control processing unit it is raised by adjusting the individual operating strength, and when the initial altitude input value is reached, the lifting fan of the rotating body is stopped and the lifting fan in the air collection body is locked and the cap is induced.
  • the speed is reduced to collect information.
  • the main body is automatically raised on the basis of external input information, so that a long time flight is possible to the information collection floating on the information collection place and path, so that high-air measurement in the shortest time, Regardless of the weather and the terrain, the role of communication relay and takeoff and landing can fly freely for a long time to collect and transmit information.
  • 1 is a configuration diagram of an unmanned information collection system floating in the air
  • Figure 2 is a perspective view of the air collection drive having an air collection cap
  • Figure 3 is a perspective view of the air collection case combined air collection body
  • FIG. 5 is a perspective view of an upper protective case constituting a three-axis gyro sensor
  • Figure 6 is a bottom view of the power supply unit coupled with the buffer support a plurality of attached to the bottom
  • FIG. 8 is a perspective view of the underside of an unmanned information gathering system floating in the air
  • FIG. 9 is a conceptual diagram illustrating the direction control according to the air flow during ascent
  • FIG. 11 is a perspective view of a wind speed processing unit and a communication relay unit coupled to a control processing unit;
  • FIG. 12 is a process diagram of a method for collecting and transmitting information while the airborne floating propulsion body is floating in the air
  • the air collection cap and air collection case of a plurality of air collection propulsion causes the air collection subunit propulsion body and the control processing body (hereinafter, the transmission and reception body) to generate more buoyancy and fall at the lowest speed.
  • Controlled by the control unit to control the rotation speed, fixed operation at a certain path and position, and at the end of the collection of various information using the device and the device that can fly in the air to return to the initial departure position It is characterized by the new concept of how it can be done.
  • the information collection processing unit 500 edits an arbitrary path, altitude, and location where information is to be collected and transmits the information to the control processing unit 200, and the received control processing unit 200 receives and stores the input and store (100-). Perform A, B). In addition, by collecting the information of the integrated (temperature / humidity / altitude / air density) sensor 41 and the GPS sensor 13 in the control processing body 200, the initial starting position and altitude are set in the storage unit and each component device Perform a process (100-C) to check whether their operation within a certain time.
  • the control strength of the control body 200 in an equilibrium state is adjusted by adjusting the operating strength for each air collection body of the air collection unit propulsion body 100 using the balance value and position information of the 3-axis gyroscope sensor 32 and the GPS sensor 13.
  • the conical air collection cap 84 of the large diameter outward and the rotary body support 83 on the air collection cap upper portion In connection with the fan central fixing part 86 fastened to the inside of the plurality of lifting fans 81 to the rotating body 82 of the central portion thereof, when the rotating body rotates and stops in one direction, the front of the lifting fan 81 faces upwards.
  • Air collection unit 80 that can be raised or lowered to lift (B-1) and air collection (C-1, C-2) to control the real-time information collected by the various sensors in the control processing body to increase and receive the main body In the liver, adjust the speed of the air drift body to raise the balance and raise .
  • the three-axis gyro sensor provides the degree of inclination of the x, y, z, axis to the control processing unit and adjusts the rotational body speed of the air collection propulsion unit in the control processing unit to achieve the balance.
  • the real-time altitude information collected by the integrated sensor altitude
  • the rotation of the rotating body is stopped, and the tilt of the lifting fan is lowered with the stop, so that the cone of the lifting fan and the air collection cap 84 is air.
  • the air collection propeller which is the shape to generate the buoyancy which is the vowels (C-1, C-2), and a plurality of such air collection propellers are fastened around the central stationary body 12, and the air collection case is covered on the top. This is increased, and the GPS sensor 13 is placed in the center together to determine the current position of the transmission and reception main body so as to collect the current position in the control processing unit.
  • the control processing unit automatically adjusts the transmitting and receiving body to fit the route, position, altitude, and time to be collected and edited by the information collection processing body, and adjusts the flight time at the corresponding point. Repeated operation allows floating transceiver body.
  • the movement (100-H) is repeated through the comparison (100-E).
  • the balloon portion 88 of a predetermined size is further connected to the upper portion of the circular central fixing body 12.
  • the lower support end 62 in which the upper support end 61 and the support scaffold 65 are vertically fastened to be connected to the support groove 64 is connected to land in order to land.
  • the buffer support 300 is fixed to the bottom of the power supply unit 50 of the control processing body 200 at a predetermined interval by fixing a plurality of buffer support 300 fixed to the tension spring 63 to attenuate the shock to cushion the shock Put it. Used to stabilize the ground at the start and landing.
  • the control processing body 200 is integrated in the center of the protective case 40 of a predetermined diameter (temperature / humidity / altitude / air density) sensor 41 and GPS sensor 13, three-axis gyro sensor 32, image sensor ( 51) and a calculation / control unit 44 which calculates and controls the values collected from the wind direction wind speed sensor 73, and stores the processed information in a storage device and transmits the information to the information collection processing unit 500 through the transmission unit 52.
  • An upper protective case 30 and a protective case which are connected to a plurality of air collection propelling bodies 80 at the upper end of the protective case 40 and fastened to the center with a 3-axis gyroscope 32 for maintaining an equilibrium state during ascending and descending.
  • a plurality of wind flow paths 71 and wind direction wind speed sensor 73 for collecting wind speed and wind direction information in the lower portion, and rotation of the inner propeller 72 to check the intensity of the winds that have entered along the wind flow paths; Fastening the wind direction processing unit 70 to collect the information of the wind direction and wind speed at a speed, and the image sensor 51, the information collection processing unit 500 for obtaining the image information in the bottom center of the wind direction wind processing unit below
  • a power supply unit 50 including a power supply unit for supplying power therein with a transmission unit 52 for transmitting the power.
  • the control processing unit 200 By comparing the current position by the control processing unit 200 for each air collection floating propellant 100 to be positioned as the initial starting point through the process to match the initial starting point, the air collection floating propellant 100 for landing
  • the air collection propulsion body of the closing of the lifting fan (81) to switch to the air collection body to descend and float to reach a certain altitude, the process of lowering the descending speed by operating the air collection floating propulsion body (100-I) and the first start If the position and altitude match, the operation of the transmitting and receiving body is terminated by stopping the measurement transmission (100-J).
  • the information collection processing unit 500 is a method and system for collecting and transmitting unmanned information floating in the air consisting of a process (100-K) of displaying, recording, storing and transmitting the collected various information to an external device.
  • A-1 Drawing wind direction by fan rotation

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Toys (AREA)

Abstract

The present invention relates to a method and system for unmanned airborne collection and transmission of information during flight, and to technology for performing an unmanned flight using an air-collecting body, descending from a predetermined altitude at an optimized speed across a set route and positions using an air-collecting cap and an air-collecting case, and transmitting collected information from sensors to an information collecting/processing body on the ground in order to record, store, and utilize the information.

Description

공중에 떠 다니는 무인 정보 수집과 송신하는 방법 및 그 시스템Method and system for collecting and transmitting unmanned information floating in the air
본 발명은 다수의 공기모음추진체를 일정각도의 반 볼록구형으로 상호 체결하여 삼각점을 형성하고, 각각의 공기모음추진체는 회전체에 연결한 다수의 원주형 팬이 중간 구동회전점을 기준으로 형성되며 일정한 방향으로 회전을 주었을 시, 원주형 팬이 일정각도로 기울어져 회전하고, 회전을 중단하고 아랫방향의 하강이 시작될 때에, 맞바람에 의해 원주형 팬의 반대방향으로 작용되어 고정단에 의한 고정체로 형성되어 아랫바람을 모아 공중부력이 생성되게 한다. The present invention forms a triangular point by fastening a plurality of air collection drive in a semi-convex sphere of a predetermined angle, each air collection drive is formed with a plurality of cylindrical fans connected to the rotating body based on the intermediate drive rotation point When the rotation is given in a certain direction, when the columnar fan is rotated by a certain angle, the rotation stops and the lower direction starts to descend, it acts in the opposite direction of the columnar fan by the upwind and is fixed to the fixed body by the fixed end. It is formed to collect the lower wind so that the buoyancy is generated.
상기 공기모음추진체와 연결되어 있고, 각 정보 수집 센서로 구성된 본체는 3축자이로센서, 온도/습도센서, 고도센서, 풍속측정단 및 이를 이용한 일정값을 정보로 전환하는 처리부, 처리된 정보를 일정한 형태로 저장, 기록하는 저장기록부와 지상에 위치하여 기상정보를 수집하는 수신부에 전송하는 전송부로 구성하며, 본체를 출발시킨 지점으로 원복할 수 있는 제어 및 조정이 되게 한다.    The main body, which is connected to the air collection propulsion unit and consists of each information collecting sensor, has a 3-axis gyroscope sensor, a temperature / humidity sensor, an altitude sensor, a wind speed measuring unit, and a processing unit for converting a predetermined value into information using the same; It is composed of a storage recorder for storing and recording in the form and a transmission unit for transmitting weather information to the receiver to collect weather information located on the ground, so that the control and adjustment that can be restored to the starting point of the main body.
일정고도까지 최대한 빠른 상승을 보장하고, 이후 일정 고도 이하로 자유낙하할 시, 양력팬을 닫아 공기모음 원추형을 생성하여 부력을 생성하여 부력을 바탕으로 하강되어 내려오는 속도를 최저로 유지하고, 보다 큰 부력을 위해 중심점을 기준으로 다수의 공기모음추진체를 결합하고 이를 상부에 케이스를 덮어 보다 큰 부력을 생성하여 공중에 떠 다니도록 한다.    As soon as possible to assure a rapid rise to a certain altitude, and after free fall below a certain altitude, the lifting fan is closed to create an air-conical cone to create a buoyancy to maintain the speed of falling down based on the buoyancy, and more Combines a large number of air collection props based on the center point for greater buoyancy and cover the case on the top to create a larger buoyancy to float in the air.
정보수집되는 장소에서의 고정, 이동 또는 선회를 위해 공기모음추진체의 회전체 회전속도를 제어처리부에서 통제하여 조정한다. 이러한 경로와 위치에서의 입력정보를 외부의 처리수신장치에서 전송하고 모든 처리가 끝나면 초기 출발된 지점으로 자동 귀환토록 하는 처리부를 둔다.The rotation speed of the rotating body of the air collection propeller is controlled and controlled by the control processor for fixing, moving or turning in the place where information is collected. Input information from these paths and locations is transmitted from an external processing receiver, and a processing unit is set up to automatically return to the starting point after all processing is completed.
최근 들어 항공 기술 및 통신 기술의 급격한 발전에 따라 탐사 및 정찰 등을 목적으로 하는 무인항공기(UAV:Unmanned Aerial Vehicle)의 개발이 활발히 이루어지고 있으며 이러한 무인 항공기는 인간이 직접 탑승하여 수행하기에 위험하거나 어려운 작업도 가능하게 하는 이점이 있다. Recently, the development of unmanned aerial vehicles (UAVs) for exploration and reconnaissance has been actively developed due to the rapid development of aviation technology and communication technology, and these drones are dangerous to be carried by humans directly. This has the advantage of enabling difficult tasks.
상기 무인항공기의 비행을 위해서는 항법장비와 속도계 및 고도계와 자세제어를 담당하는 관성항법장치(inertial navigation system)와 경로유도를 위해 GPS(Global PositioningSystem)로 이루어진다.  The flight of the unmanned aerial vehicle includes an inertial navigation system for navigation equipment, a speedometer, an altimeter, and attitude control, and a GPS (Global Positioning System) for route guidance.
상기 관성항법장치는 관성센서라 불리는 자이로스코프(Gyroscope)와 가속도계로 이루어지며, 상기 무인 항공기의 회전 각속도와 선형 가속도를 측정하여 상기 무인항공기의 현재위치, 속도, 고도, 방위각 및 비행자세에 대한 정보를 제공한다. 즉, 상기 무인항공기가 발진한 순간부터 임의의 시각까지 3축방향의 가속도를 2회 적분(積分)하면 비행거리가 얻어지며, 따라서 현재의 위치를 알 수 있다. 그러나 긴 비행시간을 위해서는 비행을 해야 하거나 회전익과 같이 항상 양력을 발생하고 있어야 하는 회전체를 구동시키고 있어야 하는 것으로 장시간의 비행은 어렵다.   The inertial navigation system consists of a gyroscope and an accelerometer called an inertial sensor, and measures the rotational angular velocity and linear acceleration of the unmanned aerial vehicle, and provides information on the current position, speed, altitude, azimuth, and flight attitude of the unmanned aerial vehicle. To provide. In other words, if the unmanned aerial vehicle is integrated two times in three-axis acceleration from the moment when the unmanned aerial vehicle starts to an arbitrary time, the flight distance is obtained, and thus the current position can be known. However, for long flight time, it is difficult to fly for a long time because it must be driven or a rotor that must always generate lift, such as a rotorcraft.
공개출원된 1020100113141 (20101020)의 비행체 (FLYING BODY)는 공기를 축류방향으로 압송하는 회전 임펠러로 이루어진 상부 송풍장치로 상부 송풍장치가 동심 형상으로 배치되는 스커트 형상의 고정익으로 이루어지며 측면의 바람의 방향을 전환하여 추력을 얻기 위한 장치로 하강되는 장치의 부력을 응용하는 방법의 원리는 아니며, 공개된 1020100016915 (20100216)의 무인항공기의 비행제어장치 및 그 제어방법 (Flight control system and control method of unmanned Aerial Vehicle) 은 항법장비, 속도계, 고도계에 발생된 고장을 인식할 수 있고, 상기 고장이 발생된 항법장비, 속도계 및 고도계에서 측정된 현재위치, 비행자세, 방위각, 속도, 고도 등을 배제하고 올바른 상기 현재위치, 비행자세, 방위각, 속도, 고도를 선택적으로 입력받을 수 있는 무인항공기의 비행제어장치 및 그 제어방법으로 비행하는 고정익 무인항공기에 대한 제어방법으로 비행체에 대한 양력을 유지하기 위한 속도계등과 같은 속력통제와 기타의 장치간의 제어방법에 대한 것으로 떠다니는 방법의 비행체를 제어하기 위한 방법은 아니다.  FLYING BODY of 1020100113141 (20101020), which is openly applied, is an upper blower composed of a rotating impeller that pumps air in an axial flow direction. The upper blower is composed of a skirt-shaped fixed blade in which the upper blower is concentrically arranged. It is not the principle of the method of applying the buoyancy of the device which is lowered to the device to obtain the thrust by switching the power, and the flight control system and control method of the unmanned aerial vehicle of the disclosed 1020100016915 (20100216) The vehicle can recognize the failure caused by the navigation equipment, the speedometer, and the altimeter, and excludes the current position, flight posture, azimuth, speed, and altitude measured by the navigation equipment, the speedometer, and the altimeter where the failure has occurred. Flight control device of unmanned aerial vehicle capable of selectively inputting current position, flight attitude, azimuth, speed, and altitude Fixed-wing method for controlling a vehicle of the way floating by on the speedometer, such as the control method between the speed control and other devices, such as for keeping the lift for the aircraft as a control method for unmanned aircraft flying to the control method is not.
상기와 같은 제한점을 개선하기 위해 정해진 경로와 위치의 상공에서 고도를 올라가거나 내려가는 작동을 지속적으로 수행할 수 있는 다수의 공기모음추진체를 사용하여 공중에 떠 다니는 방식으로 긴 비행시간을 보장하고 본체 스스로가 자동 원복할 수 있는 기능In order to improve the above limitations, a long flight time is ensured by floating in the air by using a plurality of air collecting propulsion bodies that can continuously perform the operation of raising or lowering the altitude above a predetermined path and location, and the body itself Auto-reversible function
입력되는 초기 설정 정보에 따라 일정고도까지 본체가 일정고도를 유지토록 공중에 떠 다니는 본체를 위해서 양력이 생성토록 3각 형상을 한 공기모음추진체를 통해 상승하고 고도에 따라 회전체를 정지함과 동시에 양력팬이 공기모음을 할 수 있는 각도로 전환되고 공기모음캡과 공기모음케이스에 의해 본체가 자유낙하시에도 부력이 형성되어 떠 다니도록 한다. 위치 이동과 방향 전환을 위해서 공기모음추진체별로 회전체의 회전속도를 조절할 수 있는 제어처리부를 두고 제어처리부에는 외부와 송신 및 수신할 수 있는 통신부를 둔다. According to the initial setting information input, the main body rises through the triangular-shaped air collection propulsion unit so that lift force is generated for the main body floating in the air to maintain the constant altitude up to a certain altitude, and at the same time stops the rotating body according to the altitude. Lifting fan is converted to the angle to collect the air, and the air collection cap and air collection case by the body is free buoyancy is formed floating even when free fall. For the movement of the position and the change of direction, the control processing unit can adjust the rotation speed of the rotating body for each air collection propulsion unit, and the control processing unit has a communication unit that can transmit and receive with the outside.
본체의 안전한 지상 자세제어를 위해 하단부에는 완충지지체를 두고 본체가 지형여건에 상관없이 이착륙이 되게 한다. 또한, 수집하고자 하는 용도(무인정찰, 기상측정, 통신중계 등)에 맞게 제어처리부는 모듈화시켜 결합하여 사용하는 방법으로 용도별로 결합하여 사용토록 한다. 외부에서 임의로 실시간에 사용방법을 조정할 수 있게 제어처리체에 초기 설정정보를 전송하고, 제어처리체에서 송신한 수집정보를 수신하여 표시, 처리, 저장하는 정보수집처리체를 포함한다.For the safe ground attitude control of the main body, the lower part has a buffer support so that the main body can take off and land regardless of the terrain. In addition, the control processing unit is modularized to be used in accordance with the intended use (unmanned reconnaissance, weather measurement, communication relay, etc.) to be combined and used for each purpose. And an information collecting processor for transmitting initial setting information to the control processor so as to arbitrarily adjust the usage method in real time from the outside, and receiving, displaying, processing, and storing the collected information transmitted from the control processor.
기상 및 각종 정보를 수집하기 위해 온도, 습도등의 통합된 센서를 장착하여 무게를 줄이도록 하되, 본체의 평형과 현재의 위치를 수집하기 위해 3축자이로센서 및 GPS센서를 최상의 작동을 할 수 있는 위치에 구성한다. 상부에 상승되어 있을 시에 아래에 있는 지상의 영상정보 수집을 위해서는 제어처리부의 최하단부에 영상센서를 장착하고, 상기 수집되는 각종정보를 토대로 비행자세 및 경로와 현재 위치 및 고도를 계산하여 공중에서의 자세와 위치를 조정하도록 제어처리부의 제어와 통제기능을 둔다. It is equipped with integrated sensors such as temperature and humidity to collect weather and various information to reduce the weight, but it can operate the 3-axis gyroscope and GPS sensor to collect the equilibrium and current position of the body. Configure on location. In order to collect the image information of the ground below when it is raised above, an image sensor is mounted at the bottom of the control processing unit, and the flight posture, the route, the current position and the altitude are calculated based on the collected information. Control and control functions of the control processor to adjust posture and position.
매번 최저속도로 하강하기 위해 공기모음을 할 수 있도록 구성한다. 본체를 균형되게 상승시키고 하강시에 부력을 형성할 수 있는 구조인 3각 중앙점으로 공기모음추진체 다수를 연결한 볼록형 낙하산 구조를 구성하고 회전추진유동체의 평형상태를 상시 확인하는 센서로 하여금 상승간 제어처리부에서 개별적인 작동세기 조정으로 상승시키도록 하고, 최초 설정한 고도 입력값에 도달할 시, 회전체의 양력팬 작동을 멈추며 공기모음추진체 내의 양력팬이 잠겨지며 부력을 유도되는 캡(CAP)으로 하강시 속도를 감소시켜 정보를 수집토록 한다.   It is configured to collect air to descend at the lowest speed every time. A sensor that checks the equilibrium state of the rotating propulsion fluid at all times by constructing a convex parachute structure that connects a large number of air collection propellers to a triangular center point that can raise the body in a balanced manner and form buoyancy when descending In the control processing unit, it is raised by adjusting the individual operating strength, and when the initial altitude input value is reached, the lifting fan of the rotating body is stopped and the lifting fan in the air collection body is locked and the cap is induced. When descending, the speed is reduced to collect information.
보다 큰 부력을 위해 풍선부를 결합하여 오랜시간을 공중에 떠 다니도록 한다. 제어처리부의 중간결합체를 모듈화 시켜 결합시킴으로 각종 기능을 수행하여 장시간의 공중 공간에서의 부력을 지속 유지할 수 있는 떠 다니는 비행방법과 그 시스템을 제공하는 것을 목적으로 한다.Combine the balloon for greater buoyancy so that it floats in the air for a long time. It is an object of the present invention to provide a floating flight method and a system capable of maintaining buoyancy in a long time by performing various functions by modularizing and combining an intermediate assembly of a control processing unit.
상술한 바와 같이 본 발명에 의하면, 외부의 입력되는 정보를 기초로 본체가 자동적으로 상승하고 정보수집 장소 및 경로에 떠 다니는 정보수집으로 긴 시간의 비행을 가능하게 함으로써, 최단시간내 고공기상 측정, 기상과 지형에 무관하게 통신중계 역할과 이착륙이 자유롭게 오랜시간 비행하여 정보를 수집 및 송신할 수 있는 효과가 있다.As described above, according to the present invention, the main body is automatically raised on the basis of external input information, so that a long time flight is possible to the information collection floating on the information collection place and path, so that high-air measurement in the shortest time, Regardless of the weather and the terrain, the role of communication relay and takeoff and landing can fly freely for a long time to collect and transmit information.
도 1은 공중에 떠 다니는 무인 정보수집 시스템의 구성도1 is a configuration diagram of an unmanned information collection system floating in the air
도 2는 공기모음캡을 갖는 공기모음추진체의 사시도Figure 2 is a perspective view of the air collection drive having an air collection cap
도 3은 공기모음추진체를 결합한 공기모음케이스의 사시도Figure 3 is a perspective view of the air collection case combined air collection body
도 4는 제어치리부의 내부 단면도4 is an internal cross-sectional view of the control teeth
도 5는 3축자이로센서를 구성한 상부보호케이스의 사시도5 is a perspective view of an upper protective case constituting a three-axis gyro sensor;
도 6은 밑면에 다수로 부착된 완충지지체와 결합된 전원부 밑면도Figure 6 is a bottom view of the power supply unit coupled with the buffer support a plurality of attached to the bottom
도 7은 완충지지체의 사시도7 is a perspective view of the buffer supporter
도 8은 공중에 떠 다니는 무인 정보수집 시스템의 밑면의 사시도8 is a perspective view of the underside of an unmanned information gathering system floating in the air
도 9는 상승시 공기흐름에 따른 방향조절 개념도9 is a conceptual diagram illustrating the direction control according to the air flow during ascent
도 10은 풍선부가 연결된 공중에 떠 다니는 무인 정보수집 시스템의 사시도10 is a perspective view of the unmanned information collection system floating in the air connected balloon portion
도 11은 제어처리부에 풍향풍속처리부 및 통신중계부가 체결된 사시도11 is a perspective view of a wind speed processing unit and a communication relay unit coupled to a control processing unit;
도 12은 공기모음 부유추진체가 공중에 떠 다니면서 정보 수집과 송신하는 방법의 과정도12 is a process diagram of a method for collecting and transmitting information while the airborne floating propulsion body is floating in the air
이하, 첨부된 도면을 참조하여 본 발명의 바람직한 실시예를 설명하면 다음과 같다. Hereinafter, exemplary embodiments of the present invention will be described with reference to the accompanying drawings.
다수 공기모음부유추진체를 갖는 장치로 설정하는 경로와 위치에 무인으로 일정시간 동안 떠다니며 정보를 수집하는 공중에 떠 다니는 무인 정보 수집과 송신하는 방법 및 그 시스템에 있어서; 다수의 공기모음추진체의 공기모음캡과 공기모음케이스로 하여금 공기모음부유추진체 및 제어처리체(이하, 송수신 본체)가 하강시에 보다 큰 부력이 발생하여 최저속도로 낙하토록 하고, 공기모음추진체별로 제어처리부에서 통제하여 회전속도를 조절함으로 일정경로와 위치에 고정운영하고 종료시에는 초기 출발한 위치로 회귀할 수 있도록 하는 공중에 떠 다니는 비행을 할 수 있는 장치와 그 장치를 활용하여 각종 정보를 수집할 수 있는 신개념의 방법에 특징이 있다.Claims [1] A method and system for floating and collecting unmanned information floating in the air to collect information by floating unattended for a predetermined time in a path and a location set as a device having a plurality of air collection floating body; The air collection cap and air collection case of a plurality of air collection propulsion causes the air collection subunit propulsion body and the control processing body (hereinafter, the transmission and reception body) to generate more buoyancy and fall at the lowest speed. Controlled by the control unit to control the rotation speed, fixed operation at a certain path and position, and at the end of the collection of various information using the device and the device that can fly in the air to return to the initial departure position It is characterized by the new concept of how it can be done.
정보수집처리체(500)에서 정보를 수집하고자 하는 임의의 경로, 고도와 위치를 편집하여 제어처리체(200)로 전송하고, 수신받은 제어처리체(200)는 입력 및 저장하는 과정(100-A,B)을 수행한다. 또한, 제어처리체(200)내의 통합(온도/습도/고도/공기밀도)센서(41) 및 GPS센서(13)의 정보를 수집하여 최초 출발 위치 및 고도를 저장부에 설정하고 각 구성요소 장치들의 일정시간내 작동하는 여부를 점검하는 과정(100-C)을 수행한다.  The information collection processing unit 500 edits an arbitrary path, altitude, and location where information is to be collected and transmits the information to the control processing unit 200, and the received control processing unit 200 receives and stores the input and store (100-). Perform A, B). In addition, by collecting the information of the integrated (temperature / humidity / altitude / air density) sensor 41 and the GPS sensor 13 in the control processing body 200, the initial starting position and altitude are set in the storage unit and each component device Perform a process (100-C) to check whether their operation within a certain time.
공기모음부유추진체(100)의 공기모음추진체별 작동세기를 3축자이로센서(32) 및 GPS센서(13)의 평형성 값과 위치정보를 활용해 조정하여 평형한 상태로 제어처리체(200)를 부상시키는 과정(100-D)에서 공기모음부유추진체(100)의 작동상태를 상세히 설명하면, 바깥쪽으로 직경이 큰 원추형의 공기모음캡(84)과 상기 공기모음캡 상부에 회전체지지대(83)를 두고 그 중앙부의 회전체(82)에 다수의 양력팬(81) 안쪽으로 체결한 팬중앙고정부(86)와 연결하여 회전체가 일방향으로 회전과 정지시에 양력팬(81) 전면이 상부로 올려지거나 내려져 양력(B-1)과 공기모음(C-1, C-2)을 할 수 있는 공기모음추진체(80)는 제어처리체에서 각종 센서에서 수집되는 실시간 정보를 제어하여 송수신 본체가 상승간에는 공기모음추진체의 속도를 조절하여 평형이 되게 자세를 잡고 상승한다.   The control strength of the control body 200 in an equilibrium state is adjusted by adjusting the operating strength for each air collection body of the air collection unit propulsion body 100 using the balance value and position information of the 3-axis gyroscope sensor 32 and the GPS sensor 13. Referring to the operation state of the air collection floating body 100 in the floating process (100-D) in detail, the conical air collection cap 84 of the large diameter outward and the rotary body support 83 on the air collection cap upper portion In connection with the fan central fixing part 86 fastened to the inside of the plurality of lifting fans 81 to the rotating body 82 of the central portion thereof, when the rotating body rotates and stops in one direction, the front of the lifting fan 81 faces upwards. Air collection unit 80 that can be raised or lowered to lift (B-1) and air collection (C-1, C-2) to control the real-time information collected by the various sensors in the control processing body to increase and receive the main body In the liver, adjust the speed of the air drift body to raise the balance and raise .
이때 3축 자이로센서는 x,y,z,축의 기울어짐 정도를 제어처리부에 제공하고 평형이 이루어지도록 제어처리부에서 공기모음추진체의 회전체 속도를 조정한다. 통합센서(고도)에서 수집된 실시간 고도 정보와 비교하여 일정고도에 도달하게 되면 회전체의 회전을 정지하고, 정지와 함께 양력팬의 기울기가 내려져 양력팬과 공기모음캡(84)의 원추형이 공기모음(C-1, C-2)인 부력을 생성하는 형상인 공기모음추진체가 되며 이러한 공기모음추진체가 다수개가 중앙고정체(12)를 중심으로 체결되고, 공기모음케이스가 상부에 덮혀 있어 공기모음이 증대되며, 송수신 본체의 현재 위치인지를 위해 GPS센서(13)를 함께 중앙부에 둠으로 제어처리부에 현재의 위치를 수집토록 한다.   At this time, the three-axis gyro sensor provides the degree of inclination of the x, y, z, axis to the control processing unit and adjusts the rotational body speed of the air collection propulsion unit in the control processing unit to achieve the balance. Compared with the real-time altitude information collected by the integrated sensor (altitude), when reaching a certain altitude, the rotation of the rotating body is stopped, and the tilt of the lifting fan is lowered with the stop, so that the cone of the lifting fan and the air collection cap 84 is air. It becomes the air collection propeller which is the shape to generate the buoyancy which is the vowels (C-1, C-2), and a plurality of such air collection propellers are fastened around the central stationary body 12, and the air collection case is covered on the top. This is increased, and the GPS sensor 13 is placed in the center together to determine the current position of the transmission and reception main body so as to collect the current position in the control processing unit.
지속적인 상승과 하강을 되풀이 하도록 고안하였으며, 추가로 하강시 최저 속도로 하강토록 송수신 본체 상부에 풍선부(88)를 두어 부력이 많이 생기게 한다. 정보수집처리체에서 최초 편집되어 전송된 수집해야 할 경로와 위치, 고도, 시간 등에 맞도록 제어처리부는 송수신 본체를 자동으로 조정하여 위치하게 하고 해당지점에서의 체공시간을 송수신 본체의 상승과 하강의 반복되는 작동으로 떠 다니는 송수신 본체가 되게 하였다.   It is designed to repeat the continuous ascent and descent, and additionally by placing the balloon portion 88 on the upper and lower transmission and reception body to descend at the lowest speed when the descent creates a lot of buoyancy. The control processing unit automatically adjusts the transmitting and receiving body to fit the route, position, altitude, and time to be collected and edited by the information collection processing body, and adjusts the flight time at the corresponding point. Repeated operation allows floating transceiver body.
이는 공기모음 부유 추진체(100)의 양력팬(81)을 닫아 공기모음캡과 풍선부의 부력으로 전환하여 부유 하강하는 과정(100-F) 으로 최초 입력된 값과 현재 송수신 본체가 수집하는 값과의 비교(100-E)를 통해 이동 및 정지를 되풀이(100-H) 한다. 또한, 송수신 본체가 공중에 떠 있는 시간을 최대로 하고, 하강되는 속도를 최저로 하기 위해 일정크기의 풍선부(88)를 원형 중앙고정체(12) 상부에 추가로 연결한다.   This is a process of closing the lifting fan 81 of the air collection floating propelling body 100 and converting it to the buoyancy of the air collecting cap and the balloon part to float down (100-F). The movement (100-H) is repeated through the comparison (100-E). In addition, in order to maximize the time that the transmission and reception main body in the air, and to minimize the speed of descending, the balloon portion 88 of a predetermined size is further connected to the upper portion of the circular central fixing body 12.
송수신 본체가 최초 입력된대로 수집활동이 완료되어 착륙하기 위해 상부지지단(61)과 지지발판(65)이 수직으로 체결된 하부지지단(62)을 지지체결부(64)의 연결홈으로 유동연결시키고 충격을 감쇄시키는 인장스프링(63)을 고정시킨 다수의 완충지지체(300)를 제어처리체(200)의 전원부(50) 밑면에 중앙을 기준으로 일정간격으로 고정연결하여 충격을 완화시키는 완충지지대를 둔다. 출발과 착지시에 지면에서의 자세안정을 위해 사용되어 진다.   As the transmission and reception main body is initially input, the lower support end 62 in which the upper support end 61 and the support scaffold 65 are vertically fastened to be connected to the support groove 64 is connected to land in order to land. The buffer support 300 is fixed to the bottom of the power supply unit 50 of the control processing body 200 at a predetermined interval by fixing a plurality of buffer support 300 fixed to the tension spring 63 to attenuate the shock to cushion the shock Put it. Used to stabilize the ground at the start and landing.
제어처리체(200)는 일정직경의 보호케이스(40) 중앙부에 통합(온도/습도/고도/공기밀도)센서(41) 와 GPS센서(13), 3축자이로센서(32), 영상센서(51) 및 풍향풍속확인 센서(73)로부터 수집된 값을 계산하여 제어하는 계산/제어부(44)를 두고 처리한 정보를 저장장치에 저장하고 정보수집처리체(500)로 송신부(52)를 통해 송신(100-F)할 정보를 처리하는 저장/처리부(45)와 상기 회로장치를 외부 영향을 차단하기 위한 내부보호막(43)과 전원부의 전원을 내부회로에 연결하기 위한 전원연결단(42)을 구성한다.  The control processing body 200 is integrated in the center of the protective case 40 of a predetermined diameter (temperature / humidity / altitude / air density) sensor 41 and GPS sensor 13, three-axis gyro sensor 32, image sensor ( 51) and a calculation / control unit 44 which calculates and controls the values collected from the wind direction wind speed sensor 73, and stores the processed information in a storage device and transmits the information to the information collection processing unit 500 through the transmission unit 52. A storage / processing unit 45 for processing information to be transmitted (100-F), an inner protective film 43 for blocking external effects of the circuit device, and a power connection terminal 42 for connecting the power supply of the power supply unit to the internal circuit; Configure
보호케이스(40) 상단부에 다수의 공기모음추진체(80)와 연결하고 상승과 하강시의 평형상태를 유지하기 위한 3축자이로센서(32)를 중앙부에 체결한 상부보호케이스(30) 및 보호케이스(40) 하부에 풍속과 풍향 정보를 수집하기 위한 다수의 바람유도로(71)와 풍향풍속확인 센서(73), 바람유도로를 따라 들어온 바람의 세기를 확인하기 위한 내부프로펠러(72)의 회전속도로 풍향과 풍속의 정보를 수집하는 풍향풍속처리부(70)를 체결하고, 상기 풍향풍속처리부 하부에는 밑면 중앙부에 영상정보를 획득하기 위한 영상센서(51), 정보수집처리체(500)로 정보를 송신하기 위한 송신부(52)와 내부에 전원을 공급하는 전원장치를 포함하는 전원부(50)를 체결하여 구성된다.  An upper protective case 30 and a protective case which are connected to a plurality of air collection propelling bodies 80 at the upper end of the protective case 40 and fastened to the center with a 3-axis gyroscope 32 for maintaining an equilibrium state during ascending and descending. (40) a plurality of wind flow paths 71 and wind direction wind speed sensor 73 for collecting wind speed and wind direction information in the lower portion, and rotation of the inner propeller 72 to check the intensity of the winds that have entered along the wind flow paths; Fastening the wind direction processing unit 70 to collect the information of the wind direction and wind speed at a speed, and the image sensor 51, the information collection processing unit 500 for obtaining the image information in the bottom center of the wind direction wind processing unit below And a power supply unit 50 including a power supply unit for supplying power therein with a transmission unit 52 for transmitting the power.
정보수집처리체(500)에서 최초 설정된 경로 및 고도정보를 임의로 변경하여 제어처리체(200)로 전송하여 각 센서별로 정보수집을 반복하는 과정(100-H)을 두며, 설정된 초기 출발지점과의 현재 위치를 비교하여 공기모음부유추진체(100)별로 제어처리체(200)에서 제어하여 초기 출발지점과 일치토록 하는 과정을 통해 초기 출발지점으로 위치하게 하고, 착지를 위해 공기모음부유추진체(100)의 공기모음추진체 양력팬(81)을 닫아 공기모음체로 전환하여 부유 하강하여 일정고도에 도달하면 하강속도를 공기모음부유추진체(100)를 작동시켜 하강속도를 낮추는 과정(100-I)과 최초 출발위치 및 고도와 일치하게 되면 측정 송신을 중단하는 과정(100-J)으로 송수신 본체의 작동을 종료하게 된다.  Arbitrarily change the path and altitude information initially set in the information collection processing unit 500 and transmits it to the control processing unit 200 to repeat information collection for each sensor (100-H), and with the set initial starting point. By comparing the current position by the control processing unit 200 for each air collection floating propellant 100 to be positioned as the initial starting point through the process to match the initial starting point, the air collection floating propellant 100 for landing The air collection propulsion body of the closing of the lifting fan (81) to switch to the air collection body to descend and float to reach a certain altitude, the process of lowering the descending speed by operating the air collection floating propulsion body (100-I) and the first start If the position and altitude match, the operation of the transmitting and receiving body is terminated by stopping the measurement transmission (100-J).
정보수집처리체(500)에서는 수집된 각종 정보를 표시, 기록 및 저장하고 외부장치에 전송하는 과정(100-K)으로 구성되는 공중에 떠 다니는 무인 정보 수집과 송신하는 방법과 그 시스템이다.The information collection processing unit 500 is a method and system for collecting and transmitting unmanned information floating in the air consisting of a process (100-K) of displaying, recording, storing and transmitting the collected various information to an external device.
현재까지의 가스주입식의 풍선에 의한 1회성의 고공 기상 수집을 위한 절차와 손실되는 장치를 절감할 수 있고, 무엇보다 무인으로 장시간의 비행되는 원리를 이용하여 공중에서 일정 시간동안의 정보를 수집하여 처리할 수 있거나 통신중계기와 같이 악기상과 악지형에도 구애받지 않고 실시간에 정보를 빠른 시간내 활용할 수 있는 체계가 구축됨으로 보다 장시간에 효율적인 정보수집을 필요로 하는 군사 및 기업의 효용성을 추구할 수 있어 모두 이용할 수 있을 것이다.It is possible to reduce the procedure for one-time high-air collection by the gas-injected balloon and to reduce the lost device. Above all, it collects the information for a certain period of time in the air by using the principle of flying for a long time unattended. It is possible to pursue the utility of military and companies that require efficient information collection for a long time by establishing a system that can utilize information in real time quickly regardless of musical instruments and music types such as communication repeaters. All will be available.
100 : 공기모음 부유 추진체100: air collection floating propellant
200 : 제어처리체200: control processing body
300 : 완충지지체300: buffer support
400 : 연결체400: connector
500 : 정보수집처리체500: information collection processing body
11 : 공기모음케이스11: air collection case
12 : 중앙고정체12: central fixation
13 : GPS센서13: GPS sensor
14 : 풍선부 연결고리14: balloon hook
30 : 상부보호케이스30: upper protective case
31 : 상부연결지지홈31: upper connection support groove
32 : 3축자이로센서32: 3-axis gyro sensor
40 : 보호케이스40: protective case
41 : 통합(온도/습도/고도/공기밀도) 센서41: integrated (temperature / humidity / altitude / air density) sensor
42 : 전원연결단42: power connection terminal
43 : 내부보호막43: inner protective film
44 : 계산/제어부44: calculation / control unit
45 : 저장/처리부45: storage / processing unit
50 : 전원부50: power supply
51 : 영상센서51: image sensor
52 : 송신부52: transmitter
61 : 상부지지단61: upper support end
62 : 하부지지단62: lower support end
63 : 인장스프링63: tension spring
64 : 지지체결부64: support
65 : 지지발판65: support footing
70 : 풍향풍속처리부70: wind direction processing unit
71 : 바람유도로71: wind road
72 : 내부프로펠러72: inner propeller
73 : 풍향풍속확인 센서73: wind direction sensor
80 : 공기모음추진체80: air collection drive
81 : 양력팬81: lifting fan
82 : 회전체82: rotating body
83 : 회전체지지대83: rotating body support
84 : 공기모음캡84: air collection cap
85 : 연결지지홈85: connection support groove
86 : 팬중앙고정부86: Central Fan Government
88 : 풍선부88: balloon
90 : 통신중계부90: communication relay unit
91 : 외부 다수의 송수신 안테나91: external multiple transmit and receive antenna
A-1 : 팬회전에 의한 인입바람 방향A-1: Drawing wind direction by fan rotation
A-2 : 양력A-2: Lift
B-1 : 상부부상방향B-1: Upper floating direction
C-1, C-2 : 양력팬이 정지되어 아랫방향으로 내려와 공기를 모으는 바람 이동 방향C-1, C-2: Wind moving direction where the lifting fan stops and descends downward to collect air

Claims (11)

  1. 설정하는 경로와 위치에 다수 공기모음부유추진체로 무인으로 일정시간 동안 떠다니며 정보를 수집하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템에 있어서;In the unmanned information collection and transmission in the air floating in the air for a predetermined time to collect information by a plurality of air collection floating body to the path and location to set;
    설정된 정보의 경로, 고도와 위치로 상승과 하강 및 떠 다니는 비행을 하는 공기모음부유추진체(100);, 센서로부터 수집된 정보로 공기모음팬 조정과 통제하고, 수집된 정보를 정보수집처리체(500)로 전송하는 제어처리체(200);, 상기 공기모음 부유 추진체(100)의 각 공기모음캡 밑면 끝단부의 연결지지홈(85)과 제어처리체의 상부보호케이스(30)의 상단 끝단부의 상부연결지지홈(31)을 연결하는 다수의 연결체(400);로 고정하여 형성하며, 제어처리체의 하단 전원부 밑면에 고정하여 이륙과 착륙시 충격을 완화시켜 지면에서 자세유지를 하기 위한 다수의 완충지지체(300); 및 상기 제어처리체(200)에 초기 설정정보를 전송하고, 제어처리체(200)에서 송신한 수집정보를 수신하여 표시, 처리, 저장하는 정보수집처리체(500);로 구성되는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템Air collection float propelling body (100) for the ascending and descending and floating flight of the set information path, altitude and position; Adjust and control the air collection fan with information collected from the sensor, and collects the information collected information ( The control processing body 200 to be transmitted to the; 500, the upper end of the connection support groove 85 of the bottom end of each air collection cap of the air collection floating propellant 100 and the upper protective case 30 of the control processing body A plurality of connecting bodies 400 for connecting the upper connection supporting grooves 31; and fixed to the bottom of the lower power supply portion of the control processing body to mitigate the impact during takeoff and landing to maintain posture on the ground. A buffer support 300; And an information collection processor 500 which transmits initial setting information to the control processor 200 and receives, displays, processes and stores the collection information transmitted from the control processor 200. System for collecting and transmitting unattended information
  2. 청구항 1에 있어서; The method according to claim 1;
    바깥쪽으로 직경이 큰 원추형의 공기모음캡(84)과 상기 공기모음캡 상부에 회전체지지대(83)를 두고 그 중앙부의 회전체(82)에 다수의 양력팬(81) 안쪽으로 체결한 팬중앙고정부(86)와 연결하여 회전체가 일방향으로 회전과 정지시에 양력팬(81) 전면이 상부로 올려지거나 내려져 양력과 공기모음을 할 수 있는 공기모음추진체(80);의 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템Fan central high with a conical air collecting cap 84 of large diameter outward and a rotating body support 83 on the upper air collecting cap and fastened inward to the lifting body 81 to the rotating body 82 at the center thereof. Air collection assembly (80) capable of collecting lift and air by lifting and lowering the front surface of the lifting fan (81) when the rotating body rotates and stops in one direction in connection with the government (86); System for collecting and transmitting unmanned information floating on
  3. 청구항 2에 있어서;The method according to claim 2;
    다수의 공기모음추진체(80)를 중앙고정체(12)를 중심으로 체결하여 제어처리체(200)가 일정고도까지 하강할 시, 오랜 시간 공중에 떠 있을 수 있는 공기 모음을 증대시키는 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템 When the control processing body 200 descends to a certain altitude by fastening a plurality of air collection propellers 80 around the central stationary body 12, the air collection propellant may be floated in the air for a long time. System for collecting and transmitting unmanned information floating in the air
  4. 청구항 3에 있어서; The method according to claim 3;
    일정크기의 원형 중앙고정체(12) 상단에 GPS센서(13)를 체결하여 제어처리체(200)의 현재 위치를 제어처리체(200)로 전송하는 공기모음부유추진체(100);의 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템 Includes a feature of the air collection floating body 100 for fastening the GPS sensor 13 on the top of the circular central fixed body 12 of a predetermined size to transmit the current position of the control processing body 200 to the control processing body 200. System for collecting and transmitting unmanned information floating in the air
  5. 청구항 3에 있어서; The method according to claim 3;
    다수의 공기모음추진체(80) 구성에서 체결 연결되어 형성된 공간지의 공기까지 모음을 추가하기 위해 공기모음케이스(11)을 공기모음추진체(80) 상부끝단에 결합시킨 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템Unmanned floating in the air including a feature that combines the air collection case 11 to the upper end of the air collection assembly (80) to add a collection of air space formed by fastening connection in the configuration of a plurality of air collection prop (80) Information collection and transmission system
  6. 청구항 3에 있어서; The method according to claim 3;
    제어처리체(200)이 공중에 떠 있는 시간을 최대로 하고, 하강되는 속도를 최저로 하기 위해 일정크기의 풍선부(88)를 원형 중앙고정체(12) 상부에 연결고리(14)에 연결하는 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템In order to maximize the time that the control processing body 200 is suspended in the air, and to minimize the speed of descending, the balloon 88 of a predetermined size is connected to the connecting ring 14 on the upper portion of the circular central fixing body 12. Floating unmanned information collection and transmission system containing features
  7. 청구항 1에 있어서; The method according to claim 1;
    일정직경의 보호케이스(40) 중앙부에 통합(온도/습도/고도/공기밀도)센서(41)와 GPS센서(13), 3축자이로센서(32), 영상센서(51) 및 풍향풍속확인 센서(73)로부터 수집된 값을 계산하여 제어하는 계산/제어부(44)를 두고 처리한 정보를 저장장치에 저장하고 정보수집처리체(500)로 송신할 정보를 처리하는 저장/처리부(45)와 상기 계산/제어부(44) 및 저장/처리부(45)를 외부 영향으로부터 보호하기 위한 내부보호막(43)과 전원부의 전원을 내부회로에 연결하기 위한 전원연결단(42)을 구성하고, 보호케이스(40) 상단부에 다수의 공기모음추진체(80)와 연결하고 상승과 하강시의 평형상태를 유지하기 위한 3축자이로센서(32)를 중앙부에 체결한 상부보호케이스(30) 및 보호케이스(40) 하부에 풍속과 풍향 정보를 수집하기 위한 다수의 바람유도로(71)와 풍향풍속확인 센서(73), 바람유도로를 따라 들어온 바람의 세기를 확인하기 위한 내부프로펠러(72)의 회전속도로 풍향과 풍속의 정보를 수집하는 풍향풍속처리부(70)를 체결하고, 상기 풍향풍속처리부 하부에는 밑면 중앙부에 영상정보를 획득하기 위한 영상센서(51), 정보수집처리체(500)로 정보를 송신하기 위한 송신부(52)와 내부에 전원을 공급하는 전원장치를 포함하는 전원부(50)를 체결하여 구성되는 제어처리체(200);의 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템Integrated in the center of the protective case 40 of constant diameter (temperature / humidity / altitude / air density) sensor 41, GPS sensor 13, 3-axis gyroscope sensor 32, image sensor 51 and wind direction wind speed sensor A storage / processing unit 45 for storing the processed information in a storage device and processing the information to be transmitted to the information collection processing unit 500 with a calculation / control unit 44 for calculating and controlling the values collected from the 73; An inner protective film 43 for protecting the calculation / control unit 44 and the storage / processing unit 45 from external influences, and a power connection terminal 42 for connecting the power of the power supply unit to an internal circuit, 40) The upper protective case 30 and the protective case 40 is connected to the plurality of air collection driving body 80 at the upper end and fastened the three-axis gyro sensor 32 to the center to maintain the equilibrium state during the up and down A plurality of wind induction road 71 and wind direction wind speed sensor (73) for collecting wind speed and wind direction information in the lower part, The wind direction wind speed processing unit 70 to collect the information of the wind direction and wind speed at the rotational speed of the internal propeller 72 to check the strength of the wind flows along the wind flow path, and fastened the wind direction wind processing unit in the lower part of the image at the bottom center Control configured by coupling an image sensor 51 for acquiring information, a transmitter 52 for transmitting information to the information collecting processor 500, and a power supply unit 50 including a power supply device for supplying power therein. System for collecting and transmitting unmanned information floating in the air including the characteristics of the processing body (200);
  8. 청구항 1 또는 청구항 7에 있어서; The method according to claim 1 or 7;
    외부 다수의 송수신 안테나(91)를 체결하여 특정주파수의 통신장치간 통달 거리를 연장시키도록 일정공간에 일정시간동안 주파수 중계 기능을 하는 통신중계부(90)를 체결한 제어처리체(200);의 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템A control processor (200) which has fastened a plurality of external transmitting and receiving antennas (91) to have a communication relay unit (90) functioning as a frequency relay for a predetermined time to extend a communication distance between communication devices having a specific frequency; Floating unmanned information collection and transmission system including the features of
  9. 청구항 1에 있어서; The method according to claim 1;
    상부지지단(61)과 지지발판(65)이 수직으로 체결된 하부지지단(62)을 지지체결부(64)의 연결홈으로 유동연결시키고 충격을 감쇄시키는 인장스프링(63)을 고정시킨 다수의 완충지지체(300)를 제어처리체(200)의 전원부(50) 밑면에 중앙을 기준으로 일정간격으로 고정연결하여 충격을 완화시키는 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 시스템A plurality of buffer papers in which the lower support end 62 in which the upper support end 61 and the support scaffold 65 are vertically fastened is connected to the connection groove of the support fastening portion 64, and the tension springs 63 for attenuating the shock are fixed. System for collecting and transmitting unmanned information floating in the air including a feature that mitigates the impact by fixedly connecting the retardation 300 to the bottom of the power supply unit 50 of the control processing body 200 at a predetermined interval.
  10. 설정하는 경로와 위치에 다수 공기모음부유추진체로 무인으로 일정시간 동안 떠다니며 정보를 수집 및 송신하고, 최초 출발지점으로 귀환하는 공중에 떠 다니는 무인 정보 수집과 송신하는 방법에 있어서;A method for collecting and transmitting information floating in a predetermined time by a plurality of air collection float propulsion body in a set path and location, and collecting and transmitting floating information floating in the air returning to an initial starting point;
    최고 고도, 수집경로, 운영시간의 값을 정보수집처리체(500)에서 편집/제어처리체로 전송하는 1단계(100-A); A first step (100-A) of transmitting the values of the highest altitude, the collection path, and the operating time from the information collection processing body 500 to the editing / control processing body;
    정보수집처리체(500)에 수신한 초기 설정된 정보를 제어처리체(200)에 입력 및 저장하는 2단계(100-B); Two steps (100-B) of inputting and storing the initially set information received by the information collection processing body (500) to the control processing body (200);
    제어처리체(200)의 통합(온도/습도/고도/공기밀도) 센서(41) 및 GPS센서(13)로 초기 출발 위치 및 고도를 저장부에 설정하고 각 구성요소 장치들의 일정시간내 작동하는 여부를 점검하는 3단계(100-C);Integrated control (temperature / humidity / altitude / air density) sensor 41 and GPS sensor 13 of the control processing unit 200 to set the initial starting position and altitude in the storage and operate within a certain time of each component device Three steps (100-C) to check whether there is;
    공기모음부유추진체(100)의 공기모음추진체별 작동세기를 3축자이로센서(32) 및 GPS센서(13)의 평형성 값과 위치정보를 활용해 비행조정하여 평형한 상태로 제어처리체(200)를 부상시키는 4단계(100-D);Control processing body 200 in a balanced state by adjusting the flight by using the balance value and position information of the three-axis gyro sensor 32 and GPS sensor 13 of the air collection unit propulsion body 100 of the air collection unit propulsion body 100 4 step (100-D) to injure;
    4단계의 결과로 측정되는 통합(온도/습도/고도/공기밀도)센서(41) 및 GPS센서(13)의 값에 2단계에서 설정된 설정값을 비교하는 5단계(100-E); Step 5 (100-E) comparing the set values set in step 2 to the values of the integrated (temperature / humidity / altitude / air density) sensor 41 and the GPS sensor 13 measured as the result of step 4;
    5단계의 결과 값이 설정된 값과 일치하거나 이상이면 3단계의 과정을 중단하고, 공기모음 부유 추진체(100)의 양력팬(81)을 닫아 공기모음캡과 풍선부의 부력으로 전환하여 부유 하강 및 수집되는 정보를 정보수집처리체에 전송하는 6단계(100-F);If the result value of step 5 is equal to or greater than the set value, the process of step 3 is stopped, and the lifting fan 81 of the air collection floating propellant 100 is closed to switch to the buoyancy of the air collection cap and the balloon part to lower and collect the air. Six steps (100-F) of transmitting the information to the information collection processing body;
    설정한 일정시간 및 경로를 따라 이동하며 일정고도로 부상시켜 4단계에서 6단계를 반복하는 7단계(100-H); 7 steps (100-H) of repeating steps 4 to 6 by moving along a predetermined time and path set to rise to a certain altitude;
    정보수집처리체에서 최초 설정된 경로 및 고도정보를 변경하여 7단계를 반복하고 설정된 초기 출발지점과의 현재 위치를 비교하여 공기모음부유추진체(100)를 작동시켜, 초기 출발지점과 일치토록 하는 8단계(100-G); Step 8 is repeated by changing the path and altitude information initially set in the information collection process, and comparing the current position with the set initial starting point to operate the air collection floating propulsion body 100 to make it coincide with the initial starting point. (100-G);
    6단계에서 송신되어 수신된 정보를 표시, 기록 및 저장하고 외부장치에 전송하는 9단계(100-K);Step 9 (100-K) of displaying, recording, storing and transmitting the information received and transmitted in step 6 to an external device;
    공기모음부유추진체(100)의 공기모음추진체 양력팬(81)을 닫아 공기모음체로 전환하여 부유 하강하여 일정고도에 도달하면 하강속도를 공기모음부유추진체(100)를 작동시켜 하강속도를 낮추는 10단계(100-I);10 steps to lower the descending speed by operating the descending speed to operate the air collection floating body 100 to close the air collection driving lift fan 81 of the air collection floating body 100 to switch to the air collection body to descend and float to a certain altitude (100-I);
    최초 출발위치 및 고도와 일치하게 되면 측정 송신을 중단하는 11단계(100-J); 로 구성되는 공중에 떠 다니는 무인 정보수집 및 송신하는 방법Step 11 (100-J) of stopping the transmission of the measurement when it coincides with the original starting position and altitude; Floating unmanned information collection and transmission method consisting of
  11. 청구항 10에 있어서;The method of claim 10;
    공중공간에서의 통신중계를 위해 4단계(100-D)에서 6단계(100-F)간 수신되는 특정주파수를 증폭하여 일정거리를 재송신하는 특징을 포함하는 공중에 떠 다니는 무인 정보 수집과 송신하는 방법Collecting and transmitting unmanned information floating in the air, which includes a feature of amplifying a specific frequency received between stage 4 (100-D) and stage 6 (100-F) to retransmit a certain distance for communication in the air space. Way
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