CN205203383U - Unmanned aerial vehicle image data real -time processing system - Google Patents

Unmanned aerial vehicle image data real -time processing system Download PDF

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Publication number
CN205203383U
CN205203383U CN201521049876.1U CN201521049876U CN205203383U CN 205203383 U CN205203383 U CN 205203383U CN 201521049876 U CN201521049876 U CN 201521049876U CN 205203383 U CN205203383 U CN 205203383U
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CN
China
Prior art keywords
image data
unmanned plane
time processing
processing system
data real
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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.)
Expired - Fee Related
Application number
CN201521049876.1U
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Chinese (zh)
Inventor
伍可炳
李刚
王超
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Beijing Falcon Uav Technology Co Ltd
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Beijing Falcon Uav Technology Co Ltd
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Priority to CN201521049876.1U priority Critical patent/CN205203383U/en
Application granted granted Critical
Publication of CN205203383U publication Critical patent/CN205203383U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • Processing Or Creating Images (AREA)

Abstract

The utility model provides an unmanned aerial vehicle image data real -time processing side system belongs to the information processing technology field. Unmanned aerial vehicle image data real -time processing system carries transmitter and ground satellite station's receiver including unmanned aerial vehicle, an unmanned aerial vehicle year transmitter acquire the surface map like and send the receiver for the ground satellite station with the image, receiver receive images of ground satellite station and real -time processing, its characterized in that, unmanned aerial vehicle is duct formula stationary vane oil -electricity hybrid vehicle's unmanned aerial vehicle. The utility model provides an unmanned aerial vehicle image data real -time processing side system the system can continuously shoot for a long time the surface map like.

Description

Unmanned plane image data real time processing system
Technical field
A kind of unmanned plane image data of the utility model real time processing system, belongs to technical field of target location.
Background technology
By the importance that the image of unmanned plane Real-time Obtaining terrain object is in unmanned plane operational exertion.The image of unmanned plane Real-time Obtaining terrain object has the advantages such as real-time is good, workable, is widely used in preliminary reconnaissance, real time reconnaissance, injures the uses such as assessment.From image processing point, the image of unmanned plane Real-time Obtaining terrain object is mainly used for interpretation analysis and localization process.
But unmanned plane during flying apart from not far, cruise duration is not long, is difficult to long-time photographic images.
Summary of the invention
For the deficiencies in the prior art, goal of the invention of the present utility model is to provide a kind of unmanned plane image data real time processing system, and described system can take ground image constantly for a long time.
For realizing described goal of the invention, the utility model provides one to comprise UAV system emitter and ground station receiver, UAV system emitter obtains ground image and image is sent to ground station receiver, ground station receiver receives image and process in real time, it is characterized in that, described unmanned plane is the unmanned plane of culvert type fixed-wing oil electric mixed dynamic.
Preferably, described unmanned plane is the small-sized pilotless aircraft of culvert type fixed-wing oil electric mixed dynamic, and it comprises frame 132, is provided with main duct 143 in frame 132, be provided with main blade 133 in described main duct 143, described frame 132 both sides are respectively arranged with a fixed-wing.
Preferably, be respectively arranged with little duct in the fixed-wing of frame 132 both sides, in little duct, be respectively arranged with little blade.
Preferably, the front of frame 132 and rear arrange leading edge and rear wing respectively, are respectively arranged with little duct in leading edge and rear wing, are respectively arranged with little blade in the little duct of leading edge and rear wing.
Preferably, rear wing is provided with vee tail.
Preferably, main blade provides power by fuel engines.
Preferably, little blade motor provides power, and electrical motor provides the energy by battery.
Preferably, battery is chargeable battery.
Compared with prior art, the system that provides of the utility model can photographic images constantly.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the unmanned plane image data real time processing system that the utility model provides;
Fig. 2 is the unmanned aerial vehicle contour structures schematic diagram that the utility model provides.
Detailed description of the invention
The utility model is described in detail below in conjunction with accompanying drawing.
Fig. 1 is the schematic diagram of the unmanned plane image data real time processing system that the utility model provides, as shown in Figure 1, the unmanned plane image data real time processing system that the utility model provides comprises: UAV system emitter and ground station receiver, wherein, UAV system emitter comprises CCD camera, locating module, memory device, communication module and treater (CPU), wherein, CCD camera is for obtaining the image of terrain object, and send captured image to CPU, locating module is for obtaining position data and the time data of unmanned plane, and send CPU to, CPU is used for time data, position data and view data packing framing then send communication module to, described Frame to be modulated on high-frequency signal and to send to ground station by wireless channel by communication module, memory device is for storing the operating system of data and Aerial Images emitter, also application program is stored.Ground station's Aerial Images receiver comprises ground communication module, operating unit, telltale, memory device, graphics processing unit and ground based processor (CPU), wherein, the high-frequency signal that ground communication module is sent for receiving UAV Communication module, and Frame is demodulated from high-frequency signal, then send ground CPU to, CPU separates frame take-off time data, position data and view data are also preserved in memory, graphics processing unit is used for taking out view data from memory device, and by ground CPU process, suitably be presented at telltale as required afterwards.Graphics processing unit comprises image correction unit, contour edge detecting unit and edge breakpoint joint unit.
Operating unit is such as by realizations such as keyboard, mouse, touch panel, various switches, and they enter the operating instructions for CPU earthward.Telltale is realized by read out instruments such as LCD or EL telltales, and under the control of ground CPU, display comprises the various pictures of the image frame taken by CCD.
Memory device is by the flash memory etc. of more new record can being called and storing the various IC memory devices, built-in or by the realization such as information recording carrier and reading device thereof such as hard disk, CD-ROM that digital communication terminal connects of ROM or RAM for making ground CPU carry out the program that action realizes the various functions that ground CPU possesses and the data etc. used in the execution of this program.Such as, in memory device, record the view data of the ground image obtained by communication unit.Further, also record in memory device for realizing process of the present utility model and detecting by the image processing program of the contour edge of the image rectification of localizing objects etc., contour edge, disconnecting from ground image.
Fig. 2 is the unmanned aerial vehicle contour structures schematic diagram that the utility model provides.As shown in Figure 2, the utility model unmanned aerial vehicle comprises frame 132, is provided with main duct 143 in frame 32, is provided with support 134, support 134 is provided with main blade 133 in described main duct 143.Described frame 132 both sides are respectively arranged with fixed-wing 135 and fixed-wing 136, and during flight, the fixed-wing of both sides produces aerodynamic lift, reduces the gas consumption rate of the fuel engines in main body duct.Be respectively arranged with little duct 143 and little duct 142 in the fixed-wing of frame 132 both sides, in little duct, be respectively arranged with little blade (not shown).The front and back of frame is provided with leading edge 138 and rear wing 137, is respectively arranged with little duct 141 and little duct 144, is respectively arranged with little blade (not shown) in the little duct of leading edge and rear wing 137 in leading edge 138 and rear wing 137.Rear wing is arranged empennage 129 and empennage 140, empennage 129 and empennage 140 V-shaped, in order to increase flight stability.Main blade provides power by fuel engines.Little blade motor provides power, and electrical motor provides the energy by battery.Battery is chargeable battery.Anti-twisted power flow deflector is set in culvert channel blade face, the rotating torque produced during in order to balance culvert channel blade or fan turns.Thrust flow deflector is set below culvert channel blade or fan simultaneously, produces the thrust that moves ahead.
Frame, leading edge, rear wing and empennage adopt aluminum alloy framework, and outer paving carbon fiber composite material, alleviates fuselage weight while proof strength.Support be carbon fiber bar for supporting fuel engines, as the active force of duct unmanned aerial vehicle, the fuel tank of driving engine is placed in the circumferential perimeter of main body duct.Composite propeller adopted by motor in four little ducts.
Although below done to elaborate to according to the design of the utility model object and example by reference to the accompanying drawings; but those skilled in the art will be appreciated that; under the prerequisite not departing from the utility model design, any improvement of making based on the utility model and convert the content still belonged in the utility model protection domain.

Claims (8)

1. a unmanned plane image data real time processing system, comprise UAV system emitter and ground station receiver, UAV system emitter obtains ground image and image is sent to ground station receiver, ground station receiver receives image and process in real time, it is characterized in that, described unmanned plane is the unmanned plane of culvert type fixed-wing oil electric mixed dynamic.
2. unmanned plane image data real time processing system according to claim 1, it is characterized in that, unmanned plane comprises frame (132), main duct (143) is provided with in frame (132), be provided with main blade (133) in described main duct (143), described frame (132) both sides are respectively arranged with a fixed-wing.
3. unmanned plane image data real time processing system according to claim 2, is characterized in that, is respectively arranged with little duct, is respectively arranged with little blade in little duct in the fixed-wing of frame (132) both sides.
4. unmanned plane image data real time processing system according to claim 3, it is characterized in that, front and the rear of frame (132) arrange leading edge and rear wing respectively, are respectively arranged with little duct in leading edge and rear wing, are respectively arranged with little blade in the little duct of leading edge and rear wing.
5. unmanned plane image data real time processing system according to claim 4, is characterized in that, rear wing is provided with vee tail.
6., according to the arbitrary described unmanned plane image data real time processing system of claim 1-5, it is characterized in that, main blade provides power by fuel engines.
7. unmanned plane image data real time processing system according to claim 6, it is characterized in that, little blade motor provides power, and electrical motor provides the energy by battery.
8. unmanned plane image data real time processing system according to claim 7, is characterized in that, battery is chargeable battery.
CN201521049876.1U 2015-12-17 2015-12-17 Unmanned aerial vehicle image data real -time processing system Expired - Fee Related CN205203383U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521049876.1U CN205203383U (en) 2015-12-17 2015-12-17 Unmanned aerial vehicle image data real -time processing system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521049876.1U CN205203383U (en) 2015-12-17 2015-12-17 Unmanned aerial vehicle image data real -time processing system

Publications (1)

Publication Number Publication Date
CN205203383U true CN205203383U (en) 2016-05-04

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106603979A (en) * 2016-12-14 2017-04-26 天津昕黎科技有限公司 Unmanned aerial vehicle image data real-time processing system and processing method based on electromechanics
CN108370233A (en) * 2017-08-30 2018-08-03 深圳市大疆创新科技有限公司 Detect method, equipment and the unmanned plane of photovoltaic panel
CN111532426A (en) * 2020-04-22 2020-08-14 中国空气动力研究与发展中心 Aircraft with V-shaped empennage and multiple rotors in vertical take-off and landing layout
CN111722219A (en) * 2020-07-07 2020-09-29 西安讯昂信息技术有限公司 Quick detection system of unmanned aerial vehicle ground stealth target

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106603979A (en) * 2016-12-14 2017-04-26 天津昕黎科技有限公司 Unmanned aerial vehicle image data real-time processing system and processing method based on electromechanics
CN108370233A (en) * 2017-08-30 2018-08-03 深圳市大疆创新科技有限公司 Detect method, equipment and the unmanned plane of photovoltaic panel
CN111532426A (en) * 2020-04-22 2020-08-14 中国空气动力研究与发展中心 Aircraft with V-shaped empennage and multiple rotors in vertical take-off and landing layout
CN111722219A (en) * 2020-07-07 2020-09-29 西安讯昂信息技术有限公司 Quick detection system of unmanned aerial vehicle ground stealth target

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160504