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WO2018098601A1 - Système et procédé de télésurveillance aérienne pour contrôler et surveiller des surfaces de grandes superficies - Google Patents

Système et procédé de télésurveillance aérienne pour contrôler et surveiller des surfaces de grandes superficies Download PDF

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Publication number
WO2018098601A1
WO2018098601A1 PCT/CL2016/000076 CL2016000076W WO2018098601A1 WO 2018098601 A1 WO2018098601 A1 WO 2018098601A1 CL 2016000076 W CL2016000076 W CL 2016000076W WO 2018098601 A1 WO2018098601 A1 WO 2018098601A1
Authority
WO
WIPO (PCT)
Prior art keywords
aerostat
camera
televigilance
control
images
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CL2016/000076
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English (en)
Spanish (es)
Inventor
Rodrigo Jose ALCALDE UNDURRAGA
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Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to PCT/CL2016/000076 priority Critical patent/WO2018098601A1/fr
Publication of WO2018098601A1 publication Critical patent/WO2018098601A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/40—Balloons
    • B64B1/50—Captive balloons
    • G—PHYSICS
    • G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
    • G03B37/00—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe
    • G03B37/04—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe with cameras or projectors providing touching or overlapping fields of view
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/60—Control of cameras or camera modules
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00—Television systems
    • H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast

Definitions

  • the present invention consists of a system and method of aerial televigi lancia for large surfaces, which is self-sustaining energy and capable of remotely controlling and monitoring, in real time, from anywhere and with any device with access to the network of internet, places of difficult access and that do not have a source of energy, being some of its various applications the use in agricultural operations, mining, border crossings, forestry, national parks, natural disasters, forest fires, floods, earthquakes, tidal waves, eruptions, control of causes and pollution of rivers through the use of multispectral cameras, search and rescue, massive events, road control, public and private security, or any other activity that requires the control and monitoring of large areas. It is also resistant to extreme temperatures, wind, water and allows instant access to images without requiring constant physical control. BACKGROUND OF THE INVENTION
  • drones have the advantage of offering a high displacement capacity and therefore a large field of vision, which is essential when you want to monitor or monitor large areas.
  • the drones used for these purposes offer short flight periods, in the best case of 40 minutes, depending largely on the recharging of their batteries.
  • its complicated maneuverability often makes surveillance work difficult and significantly increases accident rates, thus being considered a tool of low durability.
  • Drone Aviation Corporate firm proposed a mechanism that basically consists of tied surveillance drones, where the energy for its operation is granted by a cable from the ground and therefore its movement is only ascending and descending. It also has the disadvantage that its flight autonomy does not exceed 8 hours and requires a person in charge constantly.
  • a device that provides greater autonomy in the air than drones are aerostats.
  • These devices consist of vehicles composed of a chamber that is filled with one more gas Lightweight than air such as Helium or Hydrogen, allowing it to be suspended in the air, similar to how a Zeppelin or any other type of captive balloons works.
  • These devices are increasingly used in televigilance work as they offer long flight times, reduce accident risks compared to drones, can operate over 1 50 meters high (subject to local regulations) granting a Large field of vision and its loading capacity allows equipping them with equipment to transmit high resolution images.
  • WO 2003/053346 proposes a mobile aerial platform system comprising: an aerial platform having an outer cover, a gas containment system disposed within the outer cover , a fastening system for fixing the aerial platform to a means for transporting the system, and a payload configured to be lifted by the aerial platform when the aerial platform is inflated, where the aerial platform is configured such that It can be fully folded after being deployed.
  • US 7341224 discloses a miniature balloon for a surveillance system to be used in military and public security applications with real-time observation.
  • Video surveillance information is preprocessed and sent through wireless communication links.
  • Batteries and / or gas cylinders can be arranged to facilitate vertical movement.
  • the balloon may optionally have thrust mechanisms to facilitate lateral movements, which are fed by a source of combustible gas.
  • a drawback of the device disclosed by US 7341224 is that in order to withstand the amount of devices it carries, it requires a large volume of helium, which impairs the maneuverability of the device and significantly restricts its operation.
  • the visual and transmission technology used at the time of this document hardly allow the use of the surveillance system in any climatic condition.
  • Another existing limitation of this device is that although it allows access to the images registered from several points, the control is restricted to a single operations center, not allowing the control of camera functions from anywhere in the world.
  • US 6016998 discloses an aerial device that combines a balloon lighter than air and a kite.
  • the aerial device comprises fixing means to secure a front portion of the kite to a lower part of the globe.
  • the comet has a large portion of the nose while the balloon is shaped like an ellipsodie.
  • WO 2010/032251 also proposes an improved aerodynamic aerial platform which comprises a kite that provides a level of directional stability when raised by wind and an inflated balloon connected above the kite with a rope, with the payload attached to the kite.
  • the physical separation of the balloon with the kite isolates the payload of the shocks generated by the balloon. Additionally, insulation is provided by the use of an elastic fixing cable.
  • the electrical energy is supplied to the aerial platform by means of an optical fiber that receives power from a source located on the ground, while the conversion of the optical power to the electrical energy is carried out on board the platform.
  • the optical fiber is braided with a structure made of high tensile strength fibers.
  • the aerial platform can be loaded, for example, with a camera, batteries and transmitting elements to carry out televigilance work, among others.
  • a disadvantage of the state-of-the-art televigilance aerostatic devices is that they require access to electrical energy from the ground or be constantly lowered to the earth's surface for recharging their batteries, being unable to be energy self-sufficient and therefore involving high costs in maintenance work.
  • they often require transmission of images through cables or optical fiber, which makes it necessary to have a nearby base station, not to mention the drawbacks associated with the weight and the range limitations resulting from the presence of said cables.
  • this consists of an aerial televigilance system for monitoring large areas and energy self-sufficient.
  • This system consists mainly of an unmanned aerial unit consisting of an aerostat conformed by a hot air balloon and a comet.
  • the aerostat used is of the Helikite type, such as that disclosed in US 601 6998, which thanks to its aerostatic design is able to rise with the force of the wind and therefore lift more weight, granting more weight, granting thus a longer flight time and reducing the landing frequency for maintenance work, such as the supply of helium or hydrogen. It is also able to withstand wind speeds of up to 60 km / h, water and is made with UV resistant materials.
  • an aerostat with the aforementioned characteristics makes it possible to considerably reduce the movements, granting stability in the transmitted images, greater security, less wear of moving parts and less risk of accident. In addition, it allows to reach an operating height of 1 50 meters for at least 8 days.
  • the aerostat is equipped with multiple compartments or pockets to accommodate the last load and has in its lower part a clamping element or "Gimbal” that acts as a device that provides stability and support to some of the elements carried by the aerostat to perform Televigilance work.
  • this element consists of a flat platform made of aluminum which gives the necessary resistance with a very low weight.
  • a high resolution and low weight camera One of the elements that is fixed to the holding element of the aerostat is a high resolution and low weight camera.
  • a low-power motorized gyroscopic camera (18 to 30 W) is used, water and extreme weather resistant, preferably ONVIF (Open Network Video Interface Forum) standards, with optical, digital zoom and day vision and thermal night.
  • ONVIF Open Network Video Interface Forum
  • the camera can be configured to perform object tracking functions automatically. This quality is essential for automating the approach of a determined perimeter of so that the movements of the aerostat do not affect the perimeter recorded, thus allowing an automatic and continuous focus of the desired location.
  • the clamping element has a rocker that allows the camera to be constantly positioned and maintained at a 90 ° angle to the ground.
  • the images recorded by the camera are sent wirelessly to a control station by means of a wireless digital transmission and reception system connected to the camera, whose transmitting and receiving elements are located in the holding element of the aerostat.
  • control station is preferably located on the ground and is equipped with one or more receiving and transmitting antennas, a video receiver with a server, a digital to analog signal converter, a data transmitter, a connection device to internet and a control platform with keyboard, screen and joystick to control the specific functions of the camera and its programming from the control station.
  • Both the camera, the transmission and reception system and all electrical components arranged on the aerostat comply with IP Protection Degree according to protocol 1P66 and are electrically imposed by flexible anti-vandal photovoltaic panels of IP 66 protocol, preferably configured by two units located on the sides of the aerostat and one on the upper back, which are installed using tie-downs or other hooking elements such as Velero®.
  • the side panels are 30 W of power each and the rear panel of 100 W, also together they do not exceed 2 Kg of weight and allow generating an average daily energy close to 720 W that It is stored in batteries located in the aerostat compartments.
  • a telemetry system is also arranged on the holding element of the aerostat, which allows information about the flight status of the aerostat, such as the height, its geographical position through the incorporation of a GPS system.
  • the telemetry system also allows to know the state of charge of the batteries in real time, is small in size and is incorporated into the video signal. All this information is transmitted to the control station wirelessly by means of the transmission and reception system, which is stored on the server.
  • the server is connected to an internet connection device such as a router or similar to upload information to the web where it can be requested by the user and represented in the user interface for the display of information, configuration of parameters and the motion control and camera zoom.
  • an internet connection device such as a router or similar to upload information to the web where it can be requested by the user and represented in the user interface for the display of information, configuration of parameters and the motion control and camera zoom.
  • the image receiver of the control station receives in a single signal the images and the camera movement function that are sent from the transmitter of the aerostat, to then be sent via an Ethernet cable to the converter signal that converts the image signal of the camera into an analog format and separates it from the motion function. After this separation, each signal is again separated in two by a "Y" cable and directed on the one hand to the control platform and on the other to a digital video recorder (DVR) with server, which stores the images with an associated IP address.
  • DVR digital video recorder
  • any user can access said information remotely through software and from any part of the planet that has access to the internet network.
  • the user will have access to the recordings of the camera located in the aerostat, to control the camera and to obtain the flight telemetry data.
  • the software will transmit the signal to the camera transmitter located in the control station, which in turn is received by the receiver of the transmission and reception system of the aerostat.
  • the video and control signal of the camera provided by the software can be acquired from any appropriate user interface such as a PC, a laptop, a Tablet, a Smartphone or any similar device.
  • the transmission and reception system has a range of 5 linear kilometers (between the aerostat and the control station) without the need for direct sight.
  • the system may comprise a satellite system integrated with the server or the incorporation of high-gain military technology antennas.
  • the airborne transmission system is configured to transmit video signals and camera control along with flight telemetry directly through an internet network.
  • the aerostat is raised from a lifting base, which can be a portable inflatable station or the back of a van, or any other suitable base that avoids direct contact of the aerostat with the ground.
  • the aerostat is anchored to the ground by means of a cable wound in a winch or huinche that controls the take-off and landing manually or automatically.
  • the cable used is a low weight and resistant rope, made for example of Dynema® fiber.
  • the aerostat also has a safety device located in its front part that allows deflating the aerostat and lowering it in case of identifying abnormal movements or when an unauthorized geographical position is detected, such as more than 1500 meters from the elevation base, according to the information delivered by your gps device.
  • this consists of a method to control and monitor large areas remotely, in real time from anywhere and by any device with access to the internet network, using the system described above. Said method comprises the steps of:
  • the method comprises controlling the functions of the camera from a control module of the user interface such as the zoom, focus, position and tracking of objects and paths within a given area. , activation of laser beam to mark objects, change of lens from day to thermal or vice versa, access to previous recordings, among others.
  • the images and flight information are sent from the control center to the user interface by means of an internet signal.
  • the images and flight information are sent from the control center to the user interface by means of a satellite Italian signal.
  • the instructions for controlling camera functions from the user interface are received at the control station by means of an internet signal.
  • the instructions for controlling the functions of the camera from the user interface are received at the control station by means of a satellite signal.
  • the instructions for controlling camera functions are processed at the control station by means of the server and transmitted to the aerostat, where they are received by the wireless transmission and reception system.
  • the proposed televigilance air system and method allow to control and monitor places of difficult access and that do not have a source of energy, thus having a use in various applications such as agricultural work, mining, border crossings, events massive, road control, public and private security, or any other activity that requires the control and monitoring of large areas avoiding the need to maintain physical control.
  • the table below shows a comparison of the attributes that the system of the present invention possesses in relation to state-of-the-art technologies, which have a considerably higher surveillance cost per square meter.
  • FIG. 1 illustrates a bottom view of the proposed televigilance system aerostat.
  • FIG. 2 illustrates a side view of the proposed televigi lancia aerial system.
  • FIG. 3 illustrates a detail of the holding element of the aerostat and the components connected to it.
  • FIG. 4 and 5 illustrate a configuration of the photovoltaic panels arranged in the aerostat of the proposed television system.
  • FIG. 6 shows a scheme of communication between the devices of the proposed televigilance system.
  • FIG. 7 illustrates an example of a mobile user interface for the display and control of the camera of the proposed televigilance system.
  • the unmanned aerial unit of the proposed televigilance system consists of an aerostat 100 formed by an air balloon 101 shaped like an ellipsoid loaded with helium and a comet 102 located at the bottom of the air balloon 101, said kite 102 being formed by a horizontal upper surface 1 03 of triangular shape joined to the lower face of the hot air balloon 102 and by a triangular vertical surface 104 as a keel located at the center of the upper surface and perpendicular to it.
  • the aerostat 100 is made with UV resistant materials and according to the exemplification illustrated it has a volume of 34 m 3 and a load capacity of 1 4 Kg in windless conditions and 40 Kg with winds over 20 Km / hr .
  • the aerostat 100 is equipped with compartments or pockets 1 05 to accommodate elements such as the batteries that provide the energy for the operation of the electronic equipment, the charge controller of said batteries, the safety device for deflation of emergency and the telemetry system, said pockets 1 05 being preferably located under the upper horizontal surface 103 of the comet 102, in the upper front part of the hot air balloon 101 and in the upper face of the horizontal surface 103.
  • certain parts of the aerostat such as the triangular vertical surface 104 of the comet 102 or the upper rear face of the hot air balloon 101 provide suitable surfaces for the installation of photovoltaic panels 1 19 (see Figures 4 and 5).
  • the clamping element 1 1 0 consists of a platform made of aluminum that has a vertical plate 1 1 1 to be supported by the aerostat 1 00 and a horizontal plate 1 12 to connect the elements to hold, both plates being joined by a rocker 1 1 3 which is connected to the horizontal plate 1 12 in an oscillating manner to allow the angle of this to be varied.
  • the clamping element 1 10 supports the wireless transmission and reception system 1 15, which consists of an IP66 protocol plastic box inside which the transmitting and receiving elements are arranged. It also has supports for the 1 1 6 antennas of said elements as well as holes for the wiring of the power supply of the wireless transmission and reception system and connection with the camera and the telemetry system.
  • the box of the wireless transmission and reception system 1 1 5 is adhered to the underside of the horizontal plate 1 12 of the fastener 1 1 0, for example by means of plastic straps and / or elements such as bolts, nuts , screws, etc.
  • a high-resolution, low-weight 1 1 8 camera is fixed under the wireless transmission and reception system, for example a low-power, gyroscopic motorized camera that is resistant to water and extreme climates, with zoom Optical, digital and thermal day and night vision.
  • the chamber is fixed to the transmission and reception system box preferably by means of clamping belts 1 1 8.
  • Figures 4 and 5 illustrate a preferred arrangement of the flexible photovoltaic panels 1 1 9, of which two of them are fixed to each face of the triangular vertical surface 1 04 of the comet and a third photovoltaic panel is located at the top rear of the hot air balloon 1 01.
  • the location of the panels may vary, so that they are located anywhere in the aerostat 100 so as to seek a better exposure to the sun, which will depend on the winds in the area that place the aerostat in a certain direction.
  • the photovoltaic panels 1 19 are installed using ties 120 and / or other hooking elements such as Velero® 121 bands.
  • each photovoltaic panel 1 1 9 is connected by a cable 122 to the batteries located in the pockets 105 located under the upper horizontal surface 103 of comet 102.
  • the security system is arranged in the pocket located in the upper front part of the hot air balloon 101 to activate the deflation of the hot air balloon in case of identifying abnormal movements or when an unauthorized geographical position is detected.
  • the telemetry system (not shown) can be positioned in the clamping element 1 10, in the box of the wireless transmission and reception system 1 1 5 or in the pocket located on the upper face of the horizontal surface 103 of comet 102.
  • Said telemetry system makes it possible to gather information about the flight status of the aerostat, such as the height and its geographical position by incorporating a GPS system, as well as the battery voltage.
  • Figure 6 illustrates a diagram of the operation of the proposed televigilance system, in which it is necessary that the airborne 1 00 raised in the air records images by means of the camera installed in it, which are transmitted (a) wirelessly by means of the system of wireless transmission and reception to a control center 200 located on the ground.
  • the wireless signal emitted from the aerostat 200 is received by means of a receiving antenna 201 connected to a video receiver, a digital to analog signal converter, a server and a control platform 202, where the Information received is processed.
  • the images are uploaded to the web and accessible by a user remotely through a user interface 400 either through an internet signal (b) 300, or through a signal (c) satellite 350.
  • FIG. 7 An example of a user interface 400 is shown in Figure 7, which in the embodiment illustrated corresponds to an application for a mobile phone comprising a display module 401 for displaying in real time the images captured by the aerostat camera and a control module 402 for the user to take control of the camera and perform actions such as zoom, focus, position and object tracking.
  • the user interface 400 sends the user realized actions to the server, which are received at the control station (200) by means of a signal (b) Internet 300 or a satellite signal (c) and subsequently processed at the control center and then transmitted (a) to the air station by means of a transmitter antenna 203, where they are received by the receiver of the transmission and reception system and executed Finally in the camera.
  • the information collected by the telemetry system located in the aerostat is sent in the same way to the control center 200 for processing and availability in the user interface.

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  • Engineering & Computer Science (AREA)
  • Multimedia (AREA)
  • Signal Processing (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Studio Devices (AREA)
  • Closed-Circuit Television Systems (AREA)

Abstract

L'invention concerne un système et un procédé de télésurveillance aérienne énergétiquement autonomes pour contrôler et surveiller à distance des surfaces de grandes superficies, en temps réel, depuis n'importe quel lieu et au moyen de n'importe quel dispositif ayant accès au réseau Internet. Ledit système comprend : un aérostat (100) équipé : d'une caméra (118), d'un système d'émission et de réception sans fil (115), de panneaux photovoltaïques (119), de batteries, d'un système de charge de batteries, d'un système de télémétrie et d'un système de sécurité; une station de commande (200) qui comprend au moins une antenne réceptrice (201), un serveur et une plateforme de commande (202); et une interface utilisateur (400) qui comprend un module de visualisation (401) et un module de commande (402).
PCT/CL2016/000076 2016-12-02 2016-12-02 Système et procédé de télésurveillance aérienne pour contrôler et surveiller des surfaces de grandes superficies Ceased WO2018098601A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CL2016/000076 WO2018098601A1 (fr) 2016-12-02 2016-12-02 Système et procédé de télésurveillance aérienne pour contrôler et surveiller des surfaces de grandes superficies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CL2016/000076 WO2018098601A1 (fr) 2016-12-02 2016-12-02 Système et procédé de télésurveillance aérienne pour contrôler et surveiller des surfaces de grandes superficies

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WO2018098601A1 true WO2018098601A1 (fr) 2018-06-07

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113099149A (zh) * 2021-04-02 2021-07-09 杭州海康威视数字技术股份有限公司 一种数据处理方法、系统及存储介质
RU2828468C1 (ru) * 2024-03-14 2024-10-14 Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" Привязная территориально распределенная воздушная система технического наблюдения

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6811113B1 (en) * 2000-03-10 2004-11-02 Sky Calypso, Inc. Internet linked environmental data collection system and method
CN103414851A (zh) * 2013-07-15 2013-11-27 中国人民解放军国防科学技术大学 长航时定区域浮空监控系统
WO2015038697A2 (fr) * 2013-09-11 2015-03-19 Silicis Technologies, Inc. Remorque pour véhicule autonome
WO2015170078A2 (fr) * 2014-05-05 2015-11-12 Spillconsult Limited Plateforme aérienne captive et système d'observation aérien

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6811113B1 (en) * 2000-03-10 2004-11-02 Sky Calypso, Inc. Internet linked environmental data collection system and method
CN103414851A (zh) * 2013-07-15 2013-11-27 中国人民解放军国防科学技术大学 长航时定区域浮空监控系统
WO2015038697A2 (fr) * 2013-09-11 2015-03-19 Silicis Technologies, Inc. Remorque pour véhicule autonome
WO2015170078A2 (fr) * 2014-05-05 2015-11-12 Spillconsult Limited Plateforme aérienne captive et système d'observation aérien

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
"Asi operan los globos aerovigilantes de Santiago", AVRAM FRITCH, 21 August 2015 (2015-08-21), XP054978494, Retrieved from the Internet <URL:https://www.youtube.com/watch?v=R8QypxC34q8> [retrieved on 20170531] *
AERIAL SURVEILLANCE, 31 March 2016 (2016-03-31), XP055490523, Retrieved from the Internet <URL:http://www.helikites.com/index.php?mod=page&id_pag=60> [retrieved on 20170602] *
DESERT START HELIKITE, 13 November 2016 (2016-11-13), XP055490519, Retrieved from the Internet <URL:http://www.allsoppco.uk/index.php?mod=page&id_pag=40> [retrieved on 20170602] *
PURI, A: "A Survey of Unmanned Aerial Vehicles (UAV) for Traffic Surveillance", DEPARTMENT OF COMPUTER SCIENCE AND ENGINEERING, 2005, XP055490524, Retrieved from the Internet <URL:https://pdfs.semanticscholar.org/54f1/3fcadb405f692f8baf3b23214d811ed0f879.pdf> [retrieved on 20170531] *
THALES, EUROSATORY 2014: A TETHERED BALLOON FOR SURVEILLANCE MISSIONS, 12 June 2014 (2014-06-12), XP055490529, Retrieved from the Internet <URL:https://www.thalesgroup.com/en/worldwide/defence/news/eurosatory-2014-tethered-balloon-surveillance-missions> [retrieved on 20170531] *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113099149A (zh) * 2021-04-02 2021-07-09 杭州海康威视数字技术股份有限公司 一种数据处理方法、系统及存储介质
RU2828468C1 (ru) * 2024-03-14 2024-10-14 Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" Привязная территориально распределенная воздушная система технического наблюдения

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