CN106131491A - A kind of device for capture target - Google Patents

A kind of device for capture target Download PDF

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Publication number
CN106131491A
CN106131491A CN201610564593.3A CN201610564593A CN106131491A CN 106131491 A CN106131491 A CN 106131491A CN 201610564593 A CN201610564593 A CN 201610564593A CN 106131491 A CN106131491 A CN 106131491A
Authority
CN
China
Prior art keywords
image
subelement
starlight level
level camera
aircraft
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.)
Pending
Application number
CN201610564593.3A
Other languages
Chinese (zh)
Inventor
宋优春
宋永生
赵浩志
段国玉
尉顺超
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KEDUN SCIENCE & TECHNOLOGY Co Ltd
Original Assignee
KEDUN SCIENCE & TECHNOLOGY Co Ltd
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 KEDUN SCIENCE & TECHNOLOGY Co Ltd filed Critical KEDUN SCIENCE & TECHNOLOGY Co Ltd
Priority to CN201610564593.3A priority Critical patent/CN106131491A/en
Publication of CN106131491A publication Critical patent/CN106131491A/en
Pending legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00Television systems
    • H04N7/18Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
    • H04N7/181Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/60Control of cameras or camera modules
    • H04N23/67Focus control based on electronic image sensor signals
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/60Control of cameras or camera modules
    • H04N23/68Control of cameras or camera modules for stable pick-up of the scene, e.g. compensating for camera body vibrations
    • H04N23/682Vibration or motion blur correction
    • H04N23/684Vibration or motion blur correction performed by controlling the image sensor readout, e.g. by controlling the integration time
    • H04N23/6845Vibration or motion blur correction performed by controlling the image sensor readout, e.g. by controlling the integration time by combination of a plurality of images sequentially taken

Abstract

The present invention relates to a kind of device for capture target, belong to vehicle technology field, this device carries and uses on board the aircraft, pass through video acquisition unit, the video image of aircraft front, lower section can be absorbed, it is shown to aircraft manipulation personnel by display unit, aircraft manipulation personnel are made to will appreciate that the ambient conditions of aircraft front, lower section, and it is capable of identify that the object in the video image collected, lock onto target thing can be followed the trail of by lock onto target unit, arrest the object recognized.

Description

A kind of device for capture target
Technical field
The present invention relates to vehicle technology field, particularly to a kind of device for capture target.
Background technology
In recent decades, along with the development of science and technology, a large amount of uses of new material, aircraft has been high and new technology Masterpiece, aircraft the most progressively in the application of the field such as transport, agriculture, police, fire extinguishing, aloft flies due to it, no longer It is confined to the restriction of traditional land communications environment, therefore, is more praised highly by people.But, due to natural cause with artificial because of Aviation accident ratio that is plain and that cause is greatly increased.Nearly seventy percent accident of numerical monitor is led with artificial origin by natural cause according to statistics Cause, become the biggest obstacle of restriction aviation safety.
In flight, especially during landing, aircraft pilot is it should be understood that the ambient conditions of front and lower section, with safety Ground flight, landing.But, in prior art, aircraft does not has such equipment, so that aircraft pilot observation flight Device front and the scene of lower section.Even if some aircraft have observation front and the camera head of lower section scene, but owing to using The restriction of condition, can not preferably use, and more lacks relevant theoretical method simultaneously and instructs so that aircraft security performance Can not get being effectively improved.
It addition, the inventors discovered that, traditional arrest work and can use and arrest rifle, when rifle is arrested in use, need alert Business personnel are armed arrests suspect, owing to police are limited by surrounding, many times can not understand accurately Implement to aim at, arrest work, cause and arrest inconvenience.
Summary of the invention
Based on the problems referred to above, it is an object of the invention to overcome above-mentioned the deficiencies in the prior art, it is provided that one can be mounted in On unmanned plane can the device of capture target, make aircraft pilot can with convenient aircraft is clearly viewed in time before While the scene environment of side and lower section, capture target thing.The ultra-low illumination camera review of different focal is processed by the present invention The technology such as technology and elaborate servo control combine and come together in device, can well assisting in flying device manipulation personnel dark at night and The bad weather circumstances such as rain, snow, mist, haze descended aircraft takeoff, fly, the demand such as landing, and can capture target.
A kind of device for capture target, described device carries and uses on board the aircraft, including:
Video acquisition unit, is positioned at the lower section of aircraft, including forward sight subelement, vertical view subelement, image procossing subelement, shows Show that subelement, described forward sight subelement and described vertical view subelement are respectively used to absorb described aircraft front and described aircraft The image of lower section;Described image procossing subelement, for the image absorbed is carried out image procossing, the figure after being processed Picture;Described display subelement, the image after showing process, and from the image after described process, carry out object knowledge , it is not sent to described object image manipulate unit;
Manipulation unit, for sending lock onto target instruction according to described object image to lock onto target unit;
Lock onto target unit, for locking described object according to the instruction of described lock onto target, launches to described object and arrests Net, arrests described object.
Described forward sight subelement may include that starlight level camera lens and/or imaging lens and/or visible light lens;
Described starlight level camera lens, for gathering the starlight level image in described aircraft front;
Described imaging lens, for gathering the graphic images in described aircraft front;
Described visible light lens, for gathering the visible images in described aircraft front;
Described vertical view subelement may include that starlight level camera lens and/or imaging lens and/or visible light lens;
Described starlight level camera lens, for gathering the starlight level image below described aircraft;
Described imaging lens, for gathering the graphic images below described aircraft;
Described visible light lens, for gathering the visible images below described aircraft.
Described forward sight subelement includes the first forward sight starlight level camera lens and the second forward sight starlight level camera lens, is respectively used to picked-up The starlight level image in described aircraft front;
Described vertical view subelement includes that starlight level camera lens overlooked by the first vertical view starlight level camera lens and second, is respectively used to picked-up described Starlight level image below aircraft.
Described forward sight subelement and described vertical view subelement can be made up of independent or groups of starlight level camera lens.
Two starlight level camera lenses of described forward sight subelement are identical focal length lens, two starlights of described vertical view subelement Level is identical focal length lens;
Described image procossing subelement includes image mosaic module, for two starlight level camera lens institutes to described forward sight subelement The image absorbed carries out image mosaic, and the image being absorbed two starlight level camera lenses of described vertical view subelement carries out figure As splicing.
Two starlight level camera lenses of described forward sight subelement for differing focal length lens, two stars of described vertical view subelement Lighting level camera lens is for differing focal length lens;
Described image procossing subelement includes image co-registration module, for two starlight level camera lens institutes to described forward sight subelement The image absorbed carries out image co-registration, and the image being absorbed two starlight level camera lenses of described vertical view subelement carries out figure As merging.
Described lock onto target unit, can include the first parsing lock onto target instruction subelement, the first capture target list Unit;
Described first resolves lock onto target instruction subelement, for when receiving lock onto target instruction, resolving described locking mesh Mark instruction, obtains object information;
Described first capture target subelement, for searching for described object around described aircraft, and uses laser lamp Irradiate described object, the described object irradiated according to described laser lamp, launch arrest net to described object, arrest described Object.
Described display subelement includes:
Display module, the image after showing process;
Identify object module, for identifying object and ambient image about from the image after described process;
Sending module, for being sent to manipulation unit by described object and ambient image about;
Described manipulation unit also includes the first manipulation subelement, for generating according to described object and ambient image about Accurately lock onto target instruction, and send it to described lock onto target unit.
Described lock onto target unit includes:
Second resolves lock onto target instruction subelement, for when receiving the instruction of accurate lock onto target, resolving described accurate lock Set the goal instruction, obtains object and ambient image about;
Second capture target subelement, for according to described object and ambient image about, around described aircraft Search object and ambient image about, the ambient image around the object searched and described object respectively with Described second resolves lock onto target instruction subelement resolves the object obtained and the coupling of ambient image about, then use and swash Light modulation follows the trail of described object, launches arrest net and arrests tracked object.
Described forward sight subelement includes two 4mm starlight level camera lenses, two 8mm starlight level camera lenses, described vertical view subelement Including two 4mm starlight level camera lenses, two 8mm starlight level camera lenses, described starlight level camera lens is used for absorbing starlight level image;Described Image procossing subelement includes image mosaic module, image co-registration module, and described image mosaic module is for described forward sight The image that two 4mm starlight level camera lenses of unit are absorbed splices, two 8mm starlight level camera lenses to described forward sight unit The image absorbed splices, and the image being absorbed two 4mm starlight level camera lenses of described vertical view subelement splices, The image being absorbed two 8mm starlight level camera lenses of described vertical view unit splices;Described image co-registration module is for right Image after the image mosaic that two 4mm starlight level camera lenses of described forward sight subelement are absorbed and the two of described forward sight subelement Image after the image mosaic that individual 8mm starlight level camera lens is absorbed merges, two 4mm starlights to described vertical view subelement The image that two 8mm starlight level camera lenses of the image after the level image mosaic absorbed of camera lens and described vertical view unit are absorbed is spelled Image after connecing merges;
Described lock onto target unit includes 8mm or 12mm or 16mm starlight level camera lens, and described starlight level camera lens is used for absorbing Starlight level image.
Described video acquisition unit also includes gyroscope, servo platform, for making the shooting direction of forward sight subelement keep The shooting direction of level and vertical view subelement keeps vertically.
Described device also includes memory element, and the image after processing image procossing subelement carries out real-time storage.
Described device also includes that outdoor scene represents unit, and the image rendering being used for store in described memory element is to depositing in advance Storage is in the satellite map of described aircraft interior.
Described device also includes wireless transmission unit, for receiving the instruction that aircraft pilot sends, and instruction is sent out Give described manipulation unit;
Described manipulation unit also includes resolving instruction subelement, for resolving the instruction that described wireless transmission unit sends, and root Corresponding operating is performed according to analysis result.
The invention has the beneficial effects as follows: the video acquisition unit of the device of the capture target of the present invention, it is possible to picked-up flight Device front, the video image of lower section send display unit and are shown to aircraft manipulation personnel, enable aircraft manipulation personnel to slap Hold the ambient conditions of aircraft front, lower section, and be capable of identify that the object in the video image collected, use locking mesh Mark unit can arrest the object recognized.
Accompanying drawing explanation
Fig. 1 is a kind of device block diagram for capture target that the embodiment of the present invention provides.
Fig. 2 is the structural representation of video acquisition unit in the embodiment of the present invention.
Fig. 3 is the structural representation of lock onto target unit in the embodiment of the present invention.
Detailed description of the invention
That the following description is substantially merely exemplary and be not intended to limit the disclosure, application or purposes.Should Being understood by, in whole accompanying drawings, corresponding reference represents identical or corresponding parts and feature.
According to an aspect of the present invention, disclosing a kind of device for capture target, this device is mounted in aircraft Upper use, specific as follows:
A kind of device for capture target, reference Fig. 1, including:
Video acquisition unit 101, is positioned at the lower section of aircraft, specifically includes forward sight subelement 1011, image procossing as shown in Figure 2 Subelement 1012, vertical view subelement 1013, display subelement 1014, wherein, forward sight subelement 1011 and vertical view subelement 1013 It is respectively used to absorb the image below aircraft front and aircraft;Image procossing subelement 1012, for the figure arriving picked-up As carrying out image procossing, the image after being processed;Display subelement 1014, for showing the image after process, and from from Carrying out object identification in image after reason, this object can be to be stored in advance in this device, when display subelement 1014 When carrying out object identification, the object of the object images match that can obtain and prestore from the image after processing, will It is as the object image recognized, and is sent to this object image recognized manipulate unit 102.
Having forward sight in this device, overlook two big video acquisition unit, (display is single by display screen for aircraft pilot Unit's transmission) can the ambient conditions of clearly observation flight device front, lower section, it is ensured that the safety of flight.
In embodiments of the present invention, forward sight subelement 1011 can also include: starlight level camera lens and/or imaging lens And/or visible light lens;Wherein, starlight level camera lens, for gathering the starlight level image in aircraft front;Imaging lens, uses In the graphic images gathering aircraft front;Visible light lens, for gathering the visible images in aircraft front.Overlook son Unit 1013 may include that starlight level camera lens and/or imaging lens and/or visible light lens, wherein, starlight level camera lens, uses In gathering the starlight level image below aircraft;Imaging lens, for gathering the graphic images below aircraft;Visible ray Camera lens, for gathering the visible images below aircraft.
It addition, forward sight subelement 1011 includes the first forward sight starlight level camera lens and the second forward sight starlight level camera lens, use respectively In the starlight level image in picked-up aircraft front, overlook subelement 1013 and include that star overlooked by the first vertical view starlight level camera lens and second Lighting level camera lens, is respectively used to absorb the starlight level image below aircraft, wherein, forward sight subelement 1011 and vertical view subelement 1013 can be made up of independent or groups of starlight level camera lens.
Two starlight level camera lenses for forward sight subelement 1011 can be identical focal length lens, overlooks subelement 1013 Two starlight level camera lenses can be identical focal length lens;Image procossing subelement 1012 includes image mosaic module, for front The image absorbed depending on the starlight level camera lens of two identical focal lengths of subelement 1011 carries out image mosaic, to overlooking subelement The image that the starlight level camera lens of two identical focal lengths of 1013 is absorbed carries out image mosaic.
Two starlight level camera lenses of forward sight subelement 1011, for differing focal length lens, overlook two stars of subelement 1013 Lighting level is for differing focal length lens;Image procossing subelement 1012 includes image co-registration module, for forward sight subelement 1011 The image that absorbed of two different focal starlight level camera lenses carry out image co-registration, to two starlights overlooking subelement 1013 The image that level camera lens is absorbed carries out image co-registration.
Manipulation unit 102, for sending lock onto target instruction according to object image to lock onto target unit;
Lock onto target unit 103, for instructing lock onto target thing according to lock onto target, launches arrest net to object, arrests mesh Mark thing.Arrest net is launched to object, it is possible to reduce casualty rate during policeman's responding by lock onto target thing, it addition, this device Carry on board the aircraft, by arrest net integrated in device, more convenient tracking, capture target suspect.
In embodiments of the present invention, it is provided that one with quick lock in object, and can arrest the locking mesh of this object Mark unit 103, as it is shown on figure 3, include the first parsing lock onto target instruction subelement 1031, quick capture target subelement 1032;
First resolves lock onto target instruction subelement 1031, for when receiving lock onto target instruction, resolves lock onto target and refers to Order, obtains object information;
First capture target subelement 1032, for searching for object around aircraft, and uses laser lamp to irradiate target Thing, the object irradiated according to laser lamp, launch arrest net, capture target thing to object.
On the other hand, in embodiments of the present invention, in order to accurate capture target thing, it is to avoid arrest fall short thing or Person arrests object mistake, the cost expended when reducing capture target thing, improves the accuracy rate of capture target, video acquisition unit Display subelement 1014 in 101 includes:
Display module, the image after showing process;Identify object module, for the image after processing, identify object And ambient image about;Sending module, for being sent to manipulation unit by object and ambient image about;
Accordingly, manipulate unit 102, also include the first manipulation subelement, for according to object and ambient image about Generate the instruction of accurate lock onto target, and send it to lock onto target unit 103;
Lock onto target unit 103 can also include:
Second resolves lock onto target instruction subelement, for when receiving the instruction of accurate lock onto target, resolving and accurately lock mesh Mark instruction, obtains object and ambient image about;
Second capture target subelement, for searching for object and ambient image about, when searching around aircraft Object and object around ambient image resolve lock onto target instruction subelement respectively with second and resolve the target that obtains When thing and the coupling of ambient image about, then use laser lamp to follow the trail of object, launch arrest net, arrest tracked target Thing.
In conjunction with technique scheme, illustrate: forward sight subelement 1011 includes two 4mm starlight level camera lenses, two 8mm Starlight level camera lens, overlooks subelement 1013 and includes two 4mm starlight level camera lenses, two 8mm starlight level camera lenses, and starlight level camera lens is used In picked-up starlight level image;Image procossing subelement 1012 includes image mosaic module, image co-registration module, image mosaic module Image for being absorbed the two of forward sight subelement 1011 4mm starlight level camera lenses splices, to forward sight subelement 1011 The image that absorbed of two 8mm starlight level camera lenses splice, to two the 4mm starlight level camera lens institutes overlooking subelement 1013 The image of picked-up splices, and the image being absorbed two the 8mm starlight level camera lenses overlooking subelement 1013 splices;Figure As Fusion Module image after the image mosaic being absorbed two 4mm starlight level camera lenses of forward sight subelement 1011 is with front Merge depending on the image after the image mosaic that two 8mm starlight level camera lenses of subelement 1011 are absorbed, to overlooking subelement Image after the image mosaic that two 4mm starlight level camera lenses of 1013 are absorbed and two the 8mm starlights overlooking subelement 1013 Image after the image mosaic that level camera lens is absorbed merges;
Lock onto target unit 103 includes 8mm or 12mm or 16mm starlight level camera lens, and starlight level camera lens is used for absorbing starlight level Image.
Video acquisition unit 101 also includes gyroscope, servo platform, for making the shooting direction of forward sight subelement 1011 protect Water holding is flat and overlooks the shooting direction holding of subelement 1013 vertically.
This device also includes memory element, and the image after processing image procossing subelement 1012 is deposited in real time Storage.
It should be noted that in embodiments of the present invention, this device also includes that outdoor scene represents unit, for by memory element The image rendering of middle storage is to being stored in advance in the satellite map that this device is internal, and shows.
In order to strengthen operability, device disclosed by the invention also includes wireless transmission unit, is used for receiving aircraft and drives The instruction that the person of sailing sends, and send an instruction to manipulate unit;
Manipulation unit also includes resolving instruction subelement, for resolving the instruction that wireless transmission unit sends, and according to resolving knot Fruit performs corresponding operating.
What the contents of the section technical scheme obtained has the beneficial effect that the carry-on capture target being mounted in airflight Device gathers image about, identifies object from the image collected, and uses laser lamp to follow the trail of object, and use is grabbed Catch net capture target, thus reach the most just can launch arrest net, complete object and arrest work, reduce policeman on-the-spot The risk of injures and deaths during responding, and can aloft scout environment, search for target, hunting zone is big, little by ground no longer merely The restriction of scope, improves the efficiency of search target.Further, in the technical scheme that the present invention provides, also by different focal Ultra-low illumination photographic head with the use of, gather ambient image, first the image of identical focal length is spliced, obtains different focal Under the conditions of the spliced image of the big angle of visual field, the image of the different focal of image after above-mentioned splicing is carried out image co-registration, Ensure that the image got is clear with this, and do not affected by factors such as illumination, mist, haze, rain, snow.
A1, a kind of device for capture target, device carries and uses on board the aircraft, including:
Video acquisition unit, is positioned at the lower section of aircraft, including forward sight subelement, vertical view subelement, image procossing subelement, shows Show that subelement, forward sight subelement and vertical view subelement are respectively used to absorb the image below aircraft front and aircraft;Image Process subelement, for the image absorbed is carried out image procossing, the image after being processed;Display subelement, is used for showing Show the image after process, and the image after processing and carry out object identification, be sent to object image manipulate unit;
Manipulation unit, for sending lock onto target instruction according to object image to lock onto target unit;
Lock onto target unit, for instructing lock onto target thing according to lock onto target, launches arrest net, capture target to object Thing.
A2, device such as claim a1, it is characterised in that forward sight subelement may include that starlight level camera lens and/or heat Imaging lens and/or visible light lens;
Starlight level camera lens, for gathering the starlight level image in aircraft front;
Imaging lens, for gathering the graphic images in aircraft front;
Visible light lens, for gathering the visible images in aircraft front;
Overlook subelement and may include that starlight level camera lens and/or imaging lens and/or visible light lens;
Starlight level camera lens, for gathering the starlight level image below aircraft;
Imaging lens, for gathering the graphic images below aircraft;
Visible light lens, for gathering the visible images below aircraft.
A3, device such as claim a1, it is characterised in that forward sight subelement includes the first forward sight starlight level camera lens and Two forward sight starlight level camera lenses, are respectively used to absorb the starlight level image in aircraft front;
Overlook subelement and include that starlight level camera lens overlooked by the first vertical view starlight level camera lens and second, be respectively used to absorb under aircraft The starlight level image of side.
A4, device such as claim a1, it is characterised in that forward sight subelement with overlook subelement can be by individually or become The starlight level camera lens composition of group.
A5, device such as claim a3, it is characterised in that two starlight level camera lenses of forward sight subelement are identical focal length Camera lens, two the starlight level camera lenses overlooking subelement are identical focal length lens;
Image procossing subelement includes image mosaic module, for absorbed two starlight level camera lenses of forward sight subelement Image carries out image mosaic, and the image being absorbed two the starlight level camera lenses overlooking subelement carries out image mosaic.
A6, device such as claim a3, it is characterised in that two starlight level camera lenses of forward sight subelement are for differing Jiao Away from camera lens, overlook two starlight levels of subelement for differing focal length lens;
Image procossing subelement includes image co-registration module, for absorbed two starlight level camera lenses of forward sight subelement Image carries out image co-registration, and the image being absorbed two the starlight level camera lenses overlooking subelement carries out image co-registration.
A7, device such as claim a1, it is characterised in that lock onto target unit, can include the first parsing locking mesh Mark instruction subelement, the first capture target subelement;
First resolves lock onto target instruction subelement, for when receiving lock onto target instruction, resolves lock onto target instruction, To object information;
First capture target subelement, for searching for object around aircraft according to object information, and uses laser Light irradiation object, the object irradiated according to laser lamp, launch arrest net, capture target thing to object.
A8, device such as claim a1, it is characterised in that display subelement includes:
Display module, the image after showing process;
Identify object module, for the image after processing, identify object and ambient image about;
Sending module, for being sent to manipulation unit by object and ambient image about;
Manipulation unit also includes the first manipulation subelement, for generating accurately locking according to object and ambient image about Target instruction target word, and send it to lock onto target unit.
A9, device such as claim a8, lock onto target unit includes:
Second resolves lock onto target instruction subelement, for when receiving the instruction of accurate lock onto target, resolving and accurately lock mesh Mark instruction, obtains object and ambient image about;
Second capture target subelement, for according to object and ambient image about, searches for target around aircraft Thing and ambient image about, the ambient image around the object searched and object resolves locking with second respectively Target instruction target word subelement resolves the object obtained and the coupling of ambient image about, then use laser lamp to follow the trail of object, Launch arrest net and arrest tracked object.
A10, device such as claim a1, forward sight subelement includes two 4mm starlight level camera lenses, two 8mm starlight levels Camera lens, overlooks subelement and includes two 4mm starlight level camera lenses, two 8mm starlight level camera lenses, and starlight level camera lens is used for absorbing starlight Level image;Image procossing subelement includes image mosaic module, image co-registration module, and image mosaic module is for forward sight sub-list The image that two 4mm starlight level camera lenses of unit are absorbed splices, and is absorbed two 8mm starlight level camera lenses of forward sight unit Image splice, the image that absorbed of two 4mm starlight level camera lenses overlooking subelement is spliced, to overlooking unit The image that absorbed of two 8mm starlight level camera lenses splice;Image co-registration module is for two 4mm to forward sight subelement The image that two 8mm starlight level camera lenses of the image after the image mosaic that starlight level camera lens is absorbed and forward sight subelement are absorbed Spliced image merges, the image after the image mosaic absorbed two the 4mm starlight level camera lenses overlooking subelement Merge with the image after overlooking the image mosaic absorbed of two 8mm starlight level camera lenses of unit;
Lock onto target unit includes 8mm or 12mm or 16mm starlight level camera lens, and starlight level camera lens is used for absorbing starlight level figure Picture.
A11, device such as any one of claim a1-a10, video acquisition unit also includes gyroscope, servo platform, uses In making the shooting direction holding level of forward sight subelement and overlooking the shooting direction holding of subelement vertically.
A12, device such as any one of claim a1-a11, device also includes memory element, for image procossing Image after cell processing carries out real-time storage.
A13, device such as claim a12, device also includes that outdoor scene represents unit, for by storage in memory element Image rendering is in the satellite map being stored in advance in aircraft interior.
A14, device such as claim a1, device also includes wireless transmission unit, is used for receiving aircraft pilot and sends out The instruction sent, and send an instruction to manipulate unit;
Manipulation unit also includes resolving instruction subelement, for resolving the instruction that wireless transmission unit sends, and according to resolving knot Fruit performs corresponding operating.
It should be noted that the present invention each embodiment tetrameric all uses the mode gone forward one by one or partly repeat to describe, What each embodiment stressed is the difference with other embodiments, and between each embodiment, identical similar part is mutual See mutually.For system embodiment, due to itself and embodiment of the method basic simlarity, so describe is fairly simple, relevant Part sees the part of embodiment of the method and illustrates.
Also, it should be noted in the present invention, the relational terms of such as first and second or the like is used merely to one Individual entity or operation separate with another entity or operating space, and not necessarily require or imply these entities or operate it Between exist any this reality relation or order.And, term " includes ", " comprising " or its any other variant are intended to Contain comprising of nonexcludability, so that include that the process of a series of key element, method, article or equipment not only include those Key element, but also include other key elements being not expressly set out, or also include for this process, method, article or set Standby intrinsic key element.In the case of there is no more restriction, statement " including ... " key element limited, it is not excluded that Other identical element is there is also in including the process of described key element, method, article or equipment.
Presently disclosed embodiment, is used for making those skilled in the art realize or using the present invention.To these embodiments Multiple amendment or modification will be apparent from for a person skilled in the art.General Principle described herein can be In the case of the spirit or scope of the present invention, realize in other embodiments.Therefore, the present invention is not intended to be limited to Embodiment described herein, and it is to fit to the widest model consistent with principles disclosed herein and novel features Enclose.

Claims (10)

1. for a device for capture target, described device carries and uses on board the aircraft, it is characterised in that including:
Video acquisition unit, is positioned at the lower section of aircraft, including forward sight subelement, vertical view subelement, image procossing subelement, shows Show that subelement, described forward sight subelement and described vertical view subelement are respectively used to absorb described aircraft front and described aircraft The image of lower section;Described image procossing subelement, for the image absorbed is carried out image procossing, the figure after being processed Picture;Described display subelement, the image after showing process, and from the image after described process, carry out object knowledge , it is not sent to described object image manipulate unit;
Manipulation unit, for sending lock onto target instruction according to described object image to lock onto target unit;
Lock onto target unit, for locking described object according to the instruction of described lock onto target, launches to described object and arrests Net, arrests described object.
2. device as claimed in claim 1, it is characterised in that described forward sight subelement may include that starlight level camera lens and/or Imaging lens and/or visible light lens;
Described starlight level camera lens, for gathering the starlight level image in described aircraft front;
Described imaging lens, for gathering the graphic images in described aircraft front;
Described visible light lens, for gathering the visible images in described aircraft front;
Described vertical view subelement may include that starlight level camera lens and/or imaging lens and/or visible light lens;
Described starlight level camera lens, for gathering the starlight level image below described aircraft;
Described imaging lens, for gathering the graphic images below described aircraft;
Described visible light lens, for gathering the visible images below described aircraft.
3. device as claimed in claim 1, it is characterised in that
Described forward sight subelement includes the first forward sight starlight level camera lens and the second forward sight starlight level camera lens, is respectively used to picked-up described The starlight level image in aircraft front;
Described vertical view subelement includes that starlight level camera lens overlooked by the first vertical view starlight level camera lens and second, is respectively used to picked-up described Starlight level image below aircraft.
4. device as claimed in claim 1, it is characterised in that described forward sight subelement and described vertical view subelement can be by lists Only or groups of starlight level camera lens composition.
5. device as claimed in claim 3, it is characterised in that two starlight level camera lenses of described forward sight subelement are identical Jiao Away from camera lens, two starlight level camera lenses of described vertical view subelement are identical focal length lens;
Described image procossing subelement includes image mosaic module, for two starlight level camera lens institutes to described forward sight subelement The image absorbed carries out image mosaic, and the image being absorbed two starlight level camera lenses of described vertical view subelement carries out figure As splicing.
6. device as claimed in claim 3, it is characterised in that two starlight level camera lenses of described forward sight subelement are for differing Focal length lens, two starlight levels of described vertical view subelement are for differing focal length lens;
Described image procossing subelement includes image co-registration module, for two starlight level camera lens institutes to described forward sight subelement The image absorbed carries out image co-registration, and the image being absorbed two starlight level camera lenses of described vertical view subelement carries out figure As merging.
7. device as claimed in claim 1, it is characterised in that described lock onto target unit, can include the first parsing locking Target instruction target word subelement, the first capture target subelement;
Described first resolves lock onto target instruction subelement, for when receiving lock onto target instruction, resolving described locking mesh Mark instruction, obtains object information;
Described first capture target subelement, for searching for described target according to described object information around described aircraft Thing, and use laser lamp to irradiate described object, the described object irradiated according to described laser lamp, send out to described object Penetrate arrest net, arrest described object.
8. device as claimed in claim 1, it is characterised in that described display subelement includes:
Display module, the image after showing process;
Identify object module, for identifying object and ambient image about from the image after described process;
Sending module, for being sent to manipulation unit by described object and ambient image about;
Described manipulation unit also includes the first manipulation subelement, for generating according to described object and ambient image about Accurately lock onto target instruction, and send it to described lock onto target unit.
9. device as claimed in claim 8, it is characterised in that described lock onto target unit includes:
Second resolves lock onto target instruction subelement, for when receiving the instruction of accurate lock onto target, resolving described accurate lock Set the goal instruction, obtains object and ambient image about;
Second capture target subelement, for according to described object and ambient image about, around described aircraft Search object and ambient image about, the ambient image around the object searched and described object respectively with Described second resolves lock onto target instruction subelement resolves the object obtained and the coupling of ambient image about, then use and swash Light modulation follows the trail of described object, launches arrest net and arrests tracked object.
10. device as claimed in claim 1, it is characterised in that described forward sight subelement include two 4mm starlight level camera lenses, Two 8mm starlight level camera lenses, described vertical view subelement includes two 4mm starlight level camera lenses, two 8mm starlight level camera lenses, described Starlight level camera lens is used for absorbing starlight level image;Described image procossing subelement includes image mosaic module, image co-registration module, Described image mosaic module is spliced for the image being absorbed two 4mm starlight level camera lenses of described forward sight subelement, The image being absorbed two 8mm starlight level camera lenses of described forward sight unit splices, two to described vertical view subelement The image that 4mm starlight level camera lens is absorbed splices, the figure being absorbed two 8mm starlight level camera lenses of described vertical view unit As splicing;Described image co-registration module is for the figure being absorbed two 4mm starlight level camera lenses of described forward sight subelement As the image after the image mosaic that two 8mm starlight level camera lenses of spliced image with described forward sight subelement are absorbed is carried out Merge, the image after the image mosaic that two 4mm starlight level camera lenses of described vertical view subelement are absorbed with described overlook single Image after the image mosaic that two 8mm starlight level camera lenses of unit are absorbed merges;
Described lock onto target unit includes 8mm or 12mm or 16mm starlight level camera lens, and described starlight level camera lens is used for absorbing Starlight level image.
CN201610564593.3A 2016-07-19 2016-07-19 A kind of device for capture target Pending CN106131491A (en)

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Application publication date: 20161116