CN106357979A - Photographing method, device and terminal - Google Patents
Photographing method, device and terminal Download PDFInfo
- Publication number
- CN106357979A CN106357979A CN201610832837.1A CN201610832837A CN106357979A CN 106357979 A CN106357979 A CN 106357979A CN 201610832837 A CN201610832837 A CN 201610832837A CN 106357979 A CN106357979 A CN 106357979A
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- Prior art keywords
- star orbital
- star
- orbital
- photo
- base map
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Classifications
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- 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
- H04N23/62—Control of parameters via user interfaces
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- 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
- H04N23/667—Camera operation mode switching, e.g. between still and video, sport and normal or high- and low-resolution modes
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/80—Camera processing pipelines; Components thereof
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N5/00—Details of television systems
- H04N5/222—Studio circuitry; Studio devices; Studio equipment
- H04N5/262—Studio circuits, e.g. for mixing, switching-over, change of character of image, other special effects ; Cameras specially adapted for the electronic generation of special effects
- H04N5/2621—Cameras specially adapted for the electronic generation of special effects during image pickup, e.g. digital cameras, camcorders, video cameras having integrated special effects capability
Abstract
The invention provides a photographing method, device and terminal. The method includes: acquiring a photographing base image; performing star orbit simulation on the photographing base image according to a preset star orbit simulation mode to obtain a star orbit image. The method has the advantages that the star orbit simulation can be directly performed on the photographing base image to obtain the star orbit image; compared with a method which needs long-term photographing to obtain the star orbit image or acquires the star orbit image by synthesizing multiple photographed images in the prior art, the photographing method simplifies the photographing of the star orbit image and shortens the photographing time of the star orbit image; by the star orbit simulation according to the preset start orbit simulation mode, the ideal star orbit image can be obtained, and the photographing user experience of the start orbit image is improved.
Description
Technical field
The present invention relates to photography, more particularly, to a kind of method for imaging, device and terminal.
Background technology
Star orbital photography is always all a kind of very magical and the technology of beauty, and conventional people want to shoot the star of beauty
Rail typically requires camera terminal, dim light mirror, spider, cable release, pocket lamp, and a lot of equipment such as compass is carried out for a long time
Star orbital photography just can obtain star orbital photo；Or the photo on computers multiple being shot by way of single length exposes is carried out
Superposition just can obtain a beautiful star orbital photo.Currently not only shooting time is long for the style of shooting of this star orbital photo, shoots
Process is complicated, and the endurance of terminal is had high demands, and if not plug-in dim light mirror can be because time exposure be drawn whole
Face all overexposures are so that terminal taking star orbital effect out is often unsatisfactory；In addition, being limited to the face of end sensor
Long-pending, the factor such as quality of camera lens, even if also be difficult to take picture clearly star orbital photo using many vice-minister exposure synthesis.
Content of the invention
A kind of method for imaging provided in an embodiment of the present invention, device and terminal, mainly solving the technical problems that existing skill
The process carrying out star orbital photography in art is complicated, and time-consuming, high to demanding terminal, the star orbital photographic quality obtaining not good so that using
The bad problem of family experience.
For solving above-mentioned technical problem, the embodiment of the present invention provides a kind of method for imaging, comprising:
Obtain photography base map；
Star orbital simulation is carried out to photography base map according to default star orbital simulation model, obtains star orbital photo.
Wherein, described acquisition photography base map, comprising:
Unlatching shoot function carries out photography and obtains base map of photographing；Or
Read local picture as photography base map.
Wherein, the default star orbital simulation model of described basis carries out star orbital simulation to photography base map, obtains star orbital photo, bag
Include:
The simulation star orbital of corresponding form is added according to default star orbital simulation model on photography base map, obtains star orbital photo；
Or
According to default star orbital simulation model, the punctate opacity of the cornea on photography base map is identified, determines the punctate opacity of the cornea of star orbital to be simulated,
And star orbital simulation is carried out to the punctate opacity of the cornea of the star orbital to be simulated on photography base map, obtain star orbital photo.
Wherein, described default star orbital simulation model, at least one including in following information: star orbital simulated conditions, star orbital
Style information and star orbital regulative mode.
Wherein, the punctate opacity of the cornea of described star orbital to be simulated, comprising: pixel value meets the punctate opacity of the cornea of star orbital simulated conditions.
Wherein, also include:
Receive user operates to the adjustment of star orbital photo；
According to adjustment operation, star orbital photo is adjusted.
The present embodiment also provides a kind of photographic attachment, comprising:
Photography base map acquisition module, for obtaining photography base map；
Star orbital photo generation module, for carrying out star orbital simulation according to default star orbital simulation model to photography base map, obtains
Star orbital photo.
Wherein, star orbital photo generation module, is additionally operable to:
The simulation star orbital of corresponding form is added according to default star orbital simulation model on photography base map, obtains star orbital photo；
Or
According to default star orbital simulation model, the punctate opacity of the cornea on photography base map is identified, determines the punctate opacity of the cornea of star orbital to be simulated,
And star orbital simulation is carried out to the punctate opacity of the cornea of the star orbital to be simulated on photography base map, obtain star orbital photo.
Wherein, also include adjusting module, adjusting module is used for:
Receive user operates to the adjustment of star orbital photo；
According to adjustment operation, star orbital photo is adjusted.
The present invention also provides a kind of terminal it is characterised in that including: aforementioned photographic attachment.
The invention has the beneficial effects as follows:
Method for imaging, device and terminal that the present invention provides, by obtaining photography base map；According to default star orbital simulation model
Star orbital simulation is carried out to photography base map, obtains star orbital photo.I.e. can be after getting photography base map, directly to this photography base map
Carry out star orbital simulation, obtain star orbital photo, compared to needing in prior art to carry out shooting for a long time to obtain star orbital photo or bat
Take the photograph multiple pictures synthesis and obtain the mode of star orbital photo so that the shooting of star orbital photo becomes simple, and shorten star orbital photo
Shooting time；In addition, more preferably star orbital photo can also be obtained by star orbital simulation；Obtain star by the way
Rail photo, is integrally improved the experience that user shoots star orbital photo.
Brief description
Fig. 1 is the method for imaging flow chart of the embodiment of the present invention one；
Fig. 2 is another method for imaging flow chart of the embodiment of the present invention one；
Fig. 3 is the photographic attachment schematic diagram of the embodiment of the present invention two；
Fig. 4 is another photographic attachment schematic diagram of the embodiment of the present invention two；
Fig. 5 is the terminal schematic diagram of the embodiment of the present invention two.
Specific embodiment
Combine accompanying drawing below by specific embodiment the embodiment of the present invention is described in further detail.
Embodiment one:
The present embodiment provides a kind of method for imaging, refers to Fig. 1, specifically includes:
Step s101, obtains photography base map；
Step s102, carries out star orbital simulation according to default star orbital simulation model to described photography base map, obtains star orbital photo.
Specifically, the method for imaging that the present embodiment provides, can be direct to this photography base map after getting photography base map
Star orbital simulation is carried out according to default star orbital simulation model it is possible to obtain star orbital photo so that user can easily obtain star
Rail photo.
Wherein, for step s101, obtain photography base map, comprising: unlatching shoot function carries out photography and obtains base map of photographing；
Or read local picture as photography base map.Specifically, when obtaining photography base map, can be to need to obtain star orbital photo in user
When, open the shoot function of terminal, that is, enter exposal model, open photographic head and carry out captured in real-time and obtain this photography base map.Its
In, using the picture of captured in real-time as photography base map, taken the photograph as this including shooting the photo obtaining in the normal mode
Shadow base map, or shot by way of multiframe synthesizes, the picture that multiframe is synthesized is as this photography base map.In addition, entering
Enter exposal model carrying out image taking can be specifically that the sky to night shoots, and obtain night sky photo as this photography bottom
Figure；According to the different practical situation with sky of pixel of photographic head, the night sky photo obtaining there may be the star that can be identified
It is also possible to not have the punctate opacity of the cornea that can be identified, this punctate opacity of the cornea is star to point.It is of course also possible to be to need to obtain star orbital photograph in user
During piece, select local picture from locally stored picture as this photography base map；This local picture passes through eventually before being
Hold the picture of local photographic head shooting or download the picture storing terminal local from elsewhere.
In the present embodiment, for step s102, star orbital simulation is carried out to photography base map according to default star orbital simulation model, obtains
To star orbital photo, comprising: the simulation star orbital of corresponding form is added according to default star orbital simulation model on photography base map, obtains star
Rail photo；Or according to default star orbital simulation model, the punctate opacity of the cornea on photography base map is identified, determine the punctate opacity of the cornea of star orbital to be simulated,
And star orbital simulation is carried out to the punctate opacity of the cornea of the star orbital to be simulated on photography base map, obtain star orbital photo.
Specifically, star orbital simulation is carried out to photography base map, obtain star orbital photo, can be root after determining photography base map
The simulation star of form corresponding with this default star orbital simulation model according to default star orbital simulation model, is directly added on this photography base map
Rail, such as after obtaining photography base map, the star orbital of corresponding for default star orbital simulation model one form is directly appended to this shooting bottom
On figure, or the star orbital of corresponding for default star orbital simulation model two form is added on shooting base map.Further, can be to this
Photographs carries out image analysis, determines the position that on this photographs, sky is located, and this default star orbital simulation model is corresponded to
The star orbital of form is added to the position at sky place.Or, it is also possible to be simulated according to this default star orbital after obtaining photography base map
Pattern is identified to the punctate opacity of the cornea on this photography base map, determines the punctate opacity of the cornea of star orbital to be simulated, then further, default according to this
Star orbital simulation model carries out star orbital simulation to the punctate opacity of the cornea of star orbital to be simulated on this photography base map, and this completes the punctate opacity of the cornea of star orbital to be simulated
Star orbital simulation after photography base map be star orbital photo.
Further, the default star orbital simulation model in the present embodiment, including following information: star orbital simulated conditions, star orbital
Style information and star orbital regulative mode.Specifically, default star orbital simulation model specifically comprises star orbital simulated conditions, and this star orbital is simulated
Condition specifically includes the size information of the pixel value needing the punctate opacity of the cornea carrying out star orbital simulation, such as need in this star orbital simulated conditions into
The pixel value of the punctate opacity of the cornea of planet rail simulation is zero, then illustrate not need to carry out punctate opacity of the cornea identification, can be directly according to this default star orbital
Simulation model adds the simulation star orbital of corresponding form on photography base map, obtains star orbital photo.If needing in this star orbital simulated conditions
The pixel value carrying out the punctate opacity of the cornea of star orbital simulation is any pixel value threshold value more than zero or the pixel value range for not including zero,
Then explanation needs to carry out punctate opacity of the cornea identification, determines the punctate opacity of the cornea of star orbital to be simulated；Then according to this default star orbital simulation model to photography
On base map, the punctate opacity of the cornea of this star orbital to be simulated carries out star orbital simulation, obtains star orbital photo.Further, star to be simulated in the present embodiment
The punctate opacity of the cornea of rail, comprising: pixel value meets the punctate opacity of the cornea of star orbital simulated conditions.This default star orbital simulation mould will be more than or equal to by pixel value
The punctate opacity of the cornea of formula corresponding pixel value threshold value belongs to this default star orbital simulation mould as the punctate opacity of the cornea of this star orbital to be simulated, or by pixel value
The punctate opacity of the cornea of the corresponding pixel value range of formula is as the punctate opacity of the cornea of this star orbital to be simulated.Wherein it is determined that the punctate opacity of the cornea of star orbital to be simulated is concrete
Can be that photography base map is parsed, the pixel value of punctate opacity of the cornea respectively being identified be obtained on this photography base map, by its pixel value
Pixel value threshold value corresponding with this default star orbital simulation model is compared, or by this pixel value and this default star orbital simulation model
Corresponding pixel value is compared, and then selects pixel value to be more than or equal to the corresponding pixel value threshold value of this default star orbital simulation model
Punctate opacity of the cornea as the punctate opacity of the cornea of star orbital to be simulated, or obtain pixel value and belong to the corresponding pixel value range of this default star orbital simulation model
Punctate opacity of the cornea as star orbital to be simulated punctate opacity of the cornea.In addition, when in the present embodiment, default star orbital simulated conditions are set, can be according to reality
The factors such as the light in the actual size of punctate opacity of the cornea and photography environment in photography are specifically arranged, and are such as related to optics in photographic process
It is possible to be adjusted to this default star orbital simulated conditions according to factors such as the size of punctate opacity of the cornea and light during zoom, that is, limit really
Surely treat the pixel value threshold value of punctate opacity of the cornea or the pixel value range of star orbital adjustment, improve the accuracy of the identification of punctate opacity of the cornea treating star orbital adjustment
With the punctate opacity of the cornea rejecting the too little impact star orbital simulation effect of part.
Further, this default star orbital simulation model also includes the star orbital style information specifically simulating star orbital, this star orbital
Style information specifically includes the parameter information of setting simulation star orbital, such as simulates the center of rotation positional information of star orbital, simulates star orbital
Direction of rotation information, the length information of simulation star orbital, pitch information between simulation star orbital, the simulation shape information of star orbital and mould
Intend color information of star orbital etc..The form of simulation star orbital specifically can be set according to this default star orbital simulation model, such as permissible
Select the coordinate points on this photography base map as the center of rotation position of this simulation star orbital, or by certain on this photography base map
One object is as the center of rotation position of this simulation star orbital.Specifically, as the coordinate points of the center of rotation position of simulation star orbital
Selection Horizon line position or sky that on photography base map, sky and ground are connect can be determined according to the parsing to photography base map
The central point of the sea horizon position being connect with sea is as the center of rotation position of this simulation star orbital, or the center selecting sky
Position is as the center of rotation position of simulation star orbital；Or select on one tree or this photographic map on this photography base map
The objects such as beacon are as the center of rotation position of this simulation star orbital.In addition, this default star orbital simulation model can also include simulating
The direction of rotation information of star orbital, turns clockwise in this way, or rotate counterclockwise.This default star orbital simulation model can also include
The length information of simulation star orbital, the length information of this simulation star orbital can be specifically the simulation star orbital of all of punctate opacity of the cornea is unified
Length, or different simulation star orbital length can also be arranged as required to so that the simulation star orbital on star orbital photo is more many
Color.This default star orbital simulation model can also include simulating the pitch information between star orbital, between such as can each simulating between star orbital
Away from be identical or by simulate star orbital center of rotation position centered on, from the center of rotation position of this simulation star orbital
Spacing between more remote simulation star orbital is bigger, and the spacing between this simulation star orbital can be photographed base map according to actual needs and specifically
Aesthetic feeling specifically arrange.This default star orbital simulation model can also include simulating the shape information of star orbital, and such as this star orbital is arc
Or linear or other shapes.In addition, this default star orbital simulation model can also include simulating the color of star orbital
The color of simulation star orbital is such as set to white, yellow or blueness etc., it can be according to specific photography base map by multimedia message etc.
On the tone arranging during shooting and this photography base map, the concrete color of sky is configured.Above-mentioned specific star orbital style information can
To be arranged as required to specific parameter value it is also possible to be not provided with specific parameter value, by terminal at random to this default star orbital mould
Each parameter in simulation models is configured, and obtains random default star orbital simulation model.
Further, the default star orbital simulation model in the present embodiment also includes star orbital regulative mode, that is, include specific
The regulative mode of simulation star orbital, terminal is seen and can be coordinated the actual regulation behaviour to simulation star orbital of user by this star orbital regulative mode
This simulation star orbital of opposing is adjusted.As this star orbital regulative mode formula specially singly refers to drag the center of rotation changing simulation star orbital
Position, the mode of double finger scalings controls shape adjustment of the spacing simulating between star orbital and simulation star orbital etc..
Further, in the present embodiment, this default star orbital simulation model can just be arranged before obtaining photography base map
Alright, after getting photography base map, directly star orbital simulation is carried out to photography base map according to this default star orbital simulation model, obtain
Star orbital photo；Can also be after obtaining photography base map, need to select default star orbital corresponding with this photography base map according to user
Simulation model, then carries out star orbital simulation according to this default star orbital simulation model to this photography base map, obtains star orbital photo.
Default star orbital simulation model in the present embodiment can be just set when terminal is dispatched from the factory or root
Need to be added to terminal according to user and carry out corresponding star orbital simulation.In addition, the default star orbital simulation model in the present embodiment also may be used
Specifically to be arranged according to specific photography base map and user's request, the concrete form to this default star orbital simulation model for the present embodiment
It is not specifically limited.
Further, the method for imaging providing in the present embodiment, also includes: receive user is grasped to the adjustment of star orbital photo
Make, according to adjustment operation, star orbital photo is adjusted.I.e. after obtaining star orbital photo, if user needs to this star orbital photo
It is adjusted, then on the display interface of this star orbital photo or setting interface, this star orbital photo can also be adjusted.As with
Family can input specific adjusting parameter so that terminal adjusts on this star orbital photo according to this adjusting parameter on setting interface
Star orbital；User directly can also carry out trigger action so that terminal is according to the triggering of user on setting interface or display interface
Operation combines this star orbital photo currently corresponding default star orbital simulation model, and the simulation star orbital on this star orbital photo is adjusted
Whole.As the trigger action by being horizontally slipped on star orbital photo adjusts color and the length of star orbital, refer to scaling by double
The trigger action of form changes the concrete forms such as the shape of spacing and star orbital simulating between star orbital.In addition, providing in the present embodiment
Method for imaging, it is also possible to overall to this star orbital photo in addition to the simulation star orbital on this star orbital photo being adjusted
Be adjusted, or the other guide on this star orbital photo is adjusted it is also possible on this star orbital photo add shoot when
Between, shoot the content such as personal information.
Further, in the present embodiment, photography base map is being analyzed, during identification punctate opacity of the cornea, due to sky typically by
The situation of pure color or gradual change occurs, and can be very good to be identified；Identify a day space-time, need to other on sky such as
The objects such as bird, cloud are reasonably evaded, it is to avoid the star orbital photo obtaining is unreasonable, such as simulate bird as punctate opacity of the cornea
Its star orbital, or cloud blocked star orbital.Specifically, can be when recognizing cloud, then cloud be done hidden process, in order to avoid
Cloud masks star orbital effect, thus reaching real simulation effect.
Refer to Fig. 2, carry out a specific shooting of star orbital photograph taking according to the method for imaging that the present embodiment provides
Process specifically includes:
Step s201, clicks on photograph icon, opens shoot function.
Specifically, in the present embodiment, when needing to shoot star orbital photo, click on photograph icon, open shoot function, open
Photographic head, prepares the night sky is shot.
Step s202, selects default star orbital simulation model.
Specifically, after entering camera function, default star orbital simulation model setting options, Ke Yigen are selected on photograph interface
Select to preset accordingly star orbital simulation model according to the actual sky condition in current lens, this default star orbital simulation model can be
The fixed model having set in advance or the star orbital simulation model being arranged as required to by user；As user is permissible
Arranged in real time and obtained default star orbital simulation model, such as can be selected the pixel coverage of the specifically punctate opacity of the cornea of star orbital to be simulated,
The style of star orbital, regulative mode of star orbital etc..The pixel coverage of the punctate opacity of the cornea of this star orbital to be simulated is set greater than zero and is less than
50pixel pixel, the concrete setting of this pixel coverage can be controlled by dragging picture bar mode.Specifically can be imaged according to terminal
The actual pixels of head arrange the pixel coverage of the punctate opacity of the cornea of this star orbital to be simulated, and the such as pixel of the photographic head of terminal is 100,000～3200
Ten thousand pixels, then the pixel coverage of the punctate opacity of the cornea of this star orbital to be simulated could be arranged to aforesaid be more than zero be less than 50pixel pixel.With
When, because the pixel of terminal camera is smaller, it usually needs cooperation real-time Simulation can be only achieved optimal performance experience.In addition,
The information such as the direction of rotation that can arrange simulation star orbital, the length simulating star orbital, the regulative mode of star orbital are random model.
Step s203, presses photographic shutter, shoots and obtains star orbital photo.
Specifically, set after specifically presetting star orbital analogue model, press photographic shutter, starry sky is shot, lead to
The mode crossing multiframe synthesis obtains a base map of clearly photographing, and according to the default star orbital simulation model of aforementioned selection, this is taken the photograph
Shadow base map carries out star orbital simulation, the specific punctate opacity of the cornea being to identify star orbital to be simulated on this photography base map, enters planet to this punctate opacity of the cornea
Rail is simulated, that is, obtain star orbital photo, this star orbital photo is shown in and takes pictures on display interface.Further, being determined by user is
No needs are adjusted to this star orbital photo, to obtain final star orbital photo.
The method for imaging that the present embodiment provides, by obtaining photography base map；According to default star orbital simulation model to photography bottom
Figure carries out star orbital simulation, obtains star orbital photo.Directly star orbital can be carried out to this photography base map after getting photography base map
Simulation, obtains star orbital photo, carries out shooting for a long time compared to needs of the prior art and obtain star orbital photo or shoot multiple
Photo synthesis obtains the mode of star orbital photo so that the shooting of star orbital photo becomes simple, and shortens the shooting of star orbital photo
Time；In addition, more preferably star orbital photo can also be obtained by star orbital simulation；Obtain star orbital by the way to shine
Piece, is integrally improved the Consumer's Experience shooting star orbital photo.In addition, it is beautiful to depict a lot of by way of simulation on photo
Beautiful star orbital, it is possible to use family energy live preview shooting effect, removes wait of taking pictures for a long time from；And when simulating star orbital, use
Family can be gone the concrete form of simulation star orbital to be configured and adjusts so that the star orbital photo obtaining more conforms to according to demand
The demand of user.
Embodiment two:
The present embodiment provides a kind of photographic attachment, refers to Fig. 3, specifically includes: photography base map acquisition module 31 and star orbital
Photo generation module 32, wherein, photography base map acquisition module 31 is used for obtaining photography base map；Star orbital photo generation module 32 is used for
Star orbital simulation is carried out to photography base map according to default star orbital simulation model, obtains star orbital photo.
Specifically, the photographic attachment that the present embodiment provides, can get photography base map in photography base map acquisition module 31
Afterwards, star orbital simulation is directly carried out according to default star orbital simulation model to this photography base map by star orbital photo generation module 32 so that it may
To obtain star orbital photo so that user can easily obtain star orbital photo.
Wherein, photography base map acquisition module 31 obtains photography base map, specifically includes: unlatching shoot function carries out photography and obtains
Photography base map；Or read local picture as photography base map.Specifically, when obtaining photography base map, can be to need to obtain in user
When taking star orbital photo, open the shoot function of terminal, that is, enter exposal model, open photographic head and carry out captured in real-time and obtain this taking the photograph
Shadow base map.Can also be when user needs to obtain star orbital photo, select local picture from locally stored picture as this
Photography base map；This local picture can be the picture being shot by local photographic head before or download from elsewhere
Store local picture.
Wherein, star orbital photo generation module 32 is additionally operable to: it is right to be added on photography base map according to default star orbital simulation model
Answer the simulation star orbital of form, obtain star orbital photo；Or according to default star orbital simulation model, the punctate opacity of the cornea on photography base map is known
, do not determine the punctate opacity of the cornea of star orbital to be simulated, and star orbital simulation is carried out to the punctate opacity of the cornea of the star orbital to be simulated on photography base map, obtain star orbital
Photo.Specifically, star orbital simulation is carried out to photography base map, obtain star orbital photo, can be after determining photography base map, according to pre-
The simulation star orbital of form corresponding with this default star orbital simulation model, if star orbital simulation model, is directly added on this photography base map,
As after obtaining photography base map, the star orbital of corresponding for default star orbital simulation model one form is directly appended to this shooting base map
On, or the star orbital of corresponding for default star orbital simulation model two form is added on shooting base map.Or, obtaining base map of photographing
Afterwards it is also possible to be identified to the punctate opacity of the cornea on this photography base map according to this default star orbital simulation model, determine star orbital to be simulated
Punctate opacity of the cornea, then further, enters planet according to this default star orbital simulation model to the punctate opacity of the cornea of star orbital to be simulated on this photography base map
Rail is simulated, and the photography base map that this completes after the star orbital simulation of the punctate opacity of the cornea of simulation star orbital is star orbital photo.
Default star orbital simulation model in the present embodiment, including following information: star orbital simulated conditions, star orbital style information and
Star orbital regulative mode.Specifically, default star orbital simulation model specifically comprises star orbital simulated conditions, and this star orbital simulated conditions is specifically wrapped
Include the size of the pixel value of the punctate opacity of the cornea carrying out star orbital simulation, further, the punctate opacity of the cornea of star orbital to be simulated in the present embodiment, comprising:
Pixel value meets the punctate opacity of the cornea of star orbital simulated conditions.The corresponding pixel value of this default star orbital simulation model will be more than or equal to by pixel value
The punctate opacity of the cornea of threshold value belongs to the corresponding pixel value of this default star orbital simulation model as the punctate opacity of the cornea of this star orbital to be simulated, or by pixel value
The punctate opacity of the cornea of scope is as the punctate opacity of the cornea of this star orbital to be simulated.In addition, this default star orbital simulation model also includes specifically simulating star orbital
Star orbital style information, this star orbital style information specifically includes the parameter information of simulation star orbital setting, such as simulates the rotation of star orbital
Center location information, simulation star orbital direction of rotation information, simulation star orbital length information, simulation star orbital between pitch information,
Color information of the shape information of simulation star orbital and simulation star orbital etc..Specifically can be arranged according to this default star orbital simulation model
The form of simulation star orbital, the default star orbital simulation model in the present embodiment also includes star orbital regulative mode information, that is, include concrete
Simulation star orbital regulative mode, the actual regulation operation to simulation star orbital of user can be coordinated right by this star orbital regulative mode
Simulation star orbital is adjusted.
Further, refer to Fig. 4, the photographic attachment providing in the present embodiment, also include adjusting module 33, this adjustment mould
Block 33 is used for receive user and the adjustment of star orbital photo is operated；According to adjustment operation, star orbital photo is adjusted.Specifically,
After obtaining star orbital photo, if user is unsatisfied with to this star orbital photo or needs to be changed further, can be in star orbital photo
Display interface or setting interface on this star orbital photo is adjusted, this adjustment can be on star orbital photo simulate star orbital
Adjustment or the modification to other star orbital photo colors of itself etc..Adjusting module 33 receive user is to this star orbital
The concrete adjustment operation of photo, according to adjustment operation, is adjusted to star orbital photo.
The photographic attachment that the present embodiment provides, by obtaining photography base map；According to default star orbital simulation model to photography bottom
Figure carries out star orbital simulation, obtains star orbital photo.Directly star orbital can be carried out to this photography base map after getting photography base map
Simulation, obtains star orbital photo, carries out shooting for a long time compared to needs of the prior art and obtain star orbital photo or shoot multiple
Photo synthesis obtains the mode of star orbital photo so that the shooting of star orbital photo becomes simple, and shortens the shooting of star orbital photo
Time；In addition, more preferably star orbital photo can also be obtained by star orbital simulation；Obtain star orbital by the way to shine
Piece, is integrally improved the Consumer's Experience shooting star orbital photo.In addition, it is beautiful to depict a lot of by way of simulation on photo
Beautiful star orbital, it is possible to use family energy live preview shooting effect, removes wait of taking pictures for a long time from；And when simulating star orbital, use
Family can be gone the concrete form of simulation star orbital to be configured and adjusts so that the star orbital photo obtaining more conforms to according to demand
The demand of user.
The present invention also provides a kind of terminal, refers to Fig. 5, including aforementioned photographic attachment.The terminal that the present embodiment provides, leads to
Cross and aforesaid photographic attachment is set, can be by star orbital simulation being carried out to the photography base map getting it is possible to synthesis obtains star
Rail photo, passes through long exposure plus-minus light microscopic compared to terminal of the prior art and shoots to obtain multiple stellar maps, then to this multiple
Stellar map is overlapped obtaining the mode of star orbital photo, shortens the generation time of this star orbital photo, and the life of star orbital photo
During one-tenth, the requirement to the endurance of this terminal, end sensor and photographic head is not also high so that user passes through this terminal
Just can easily and efficiently shoot preferable star orbital photo, the star orbital photo that user can also be generated by this terminal-pair enters
Row is adjusted, and makes star orbital photo more meet user's request.The present embodiment provide terminal can be with camera function or image at
The photographing unit of reason function, mobile phone, panel computer or pc (personal computer, personal computer) etc..
Above content is the further description embodiment of the present invention made with reference to specific embodiment it is impossible to recognize
Determine the present invention be embodied as be confined to these explanations.For general technical staff of the technical field of the invention,
Without departing from the inventive concept of the premise, some simple deduction or replace can also be made, all should be considered as belonging to the present invention
Protection domain.
Claims (10)
1. a kind of method for imaging is it is characterised in that include:
Obtain photography base map；
Star orbital simulation is carried out to described photography base map according to default star orbital simulation model, obtains star orbital photo.
2. method for imaging as claimed in claim 1 it is characterised in that described acquisition photography base map, comprising:
Unlatching shoot function carries out photography and obtains described photography base map；Or
Read local picture as described photography base map.
3. method for imaging as claimed in claim 1 is it is characterised in that described basis presets star orbital simulation model to described photography
Base map carries out star orbital simulation, obtains star orbital photo, comprising:
The simulation star orbital of corresponding form is added according to described default star orbital simulation model on described photography base map, obtains described star
Rail photo；Or
According to described default star orbital simulation model, the punctate opacity of the cornea on described photography base map is identified, determines the star of star orbital to be simulated
Point, and star orbital simulation is carried out to the punctate opacity of the cornea of star orbital to be simulated described on described photography base map, obtain described star orbital photo.
4. method for imaging as claimed in claim 1 is it is characterised in that described default star orbital simulation model, including following information
In at least one: star orbital simulated conditions, star orbital style information and star orbital regulative mode.
5. method for imaging as claimed in claim 4 is it is characterised in that the punctate opacity of the cornea of described star orbital to be simulated, comprising: pixel value is full
The punctate opacity of the cornea of the described star orbital simulated conditions of foot.
6. the method for imaging as described in any one of claim 1-5 is it is characterised in that also include:
Receive user operates to the adjustment of described star orbital photo；
According to described adjustment operation, described star orbital photo is adjusted.
7. a kind of photographic attachment is it is characterised in that include:
Photography base map acquisition module, for obtaining photography base map；
Star orbital photo generation module, for carrying out star orbital simulation according to default star orbital simulation model to described photography base map, obtains
Star orbital photo.
8. photographic attachment as claimed in claim 7, it is characterised in that described star orbital photo generation module, is additionally operable to:
The simulation star orbital of corresponding form is added according to described default star orbital simulation model on described photography base map, obtains described star
Rail photo；Or
According to described default star orbital simulation model, the punctate opacity of the cornea on described photography base map is identified, determines the star of star orbital to be simulated
Point, and star orbital simulation is carried out to the punctate opacity of the cornea of star orbital to be simulated described on described photography base map, obtain described star orbital photo.
9. photographic attachment as claimed in claim 7 or 8 it is characterised in that also including adjusting module, use by described adjusting module
In:
Receive user operates to the adjustment of described star orbital photo；
According to described adjustment operation, described star orbital photo is adjusted.
10. a kind of terminal is it is characterised in that include: the photographic attachment as described in any one of claim 7-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610832837.1A CN106357979A (en) | 2016-09-19 | 2016-09-19 | Photographing method, device and terminal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610832837.1A CN106357979A (en) | 2016-09-19 | 2016-09-19 | Photographing method, device and terminal |
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| CN106357979A true CN106357979A (en) | 2017-01-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610832837.1A Pending CN106357979A (en) | 2016-09-19 | 2016-09-19 | Photographing method, device and terminal |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107071278A (en) * | 2017-03-31 | 2017-08-18 | 努比亚技术有限公司 | Terminal and star orbital shooting method |
| CN110930329A (en) * | 2019-11-20 | 2020-03-27 | 维沃移动通信有限公司 | Starry sky image processing method and device |
| CN111010511A (en) * | 2019-12-12 | 2020-04-14 | 维沃移动通信有限公司 | Panoramic body-separating image shooting method and electronic equipment |
| CN112351207A (en) * | 2020-10-30 | 2021-02-09 | 维沃移动通信有限公司 | Shooting control method and electronic equipment |
| CN112399078A (en) * | 2020-10-30 | 2021-02-23 | 维沃移动通信有限公司 | Shooting method and device and electronic equipment |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101226113A (en) * | 2008-01-30 | 2008-07-23 | 北京航空航天大学 | Method and apparatus for testing star sensor function based on electric injection star map |
| CN102694967A (en) * | 2011-03-22 | 2012-09-26 | 天津三星光电子有限公司 | A star gazing-realizing method and a device thereof |
| CN102759348A (en) * | 2012-07-18 | 2012-10-31 | 宁波舜宇电子有限公司 | System for automatically identifying coordinates of shooting sites by using star-field digital photography |
| CN103905730A (en) * | 2014-03-24 | 2014-07-02 | 深圳市中兴移动通信有限公司 | Shooting method of mobile terminal and mobile terminal |
| CN104079833A (en) * | 2014-07-02 | 2014-10-01 | 深圳市中兴移动通信有限公司 | Method and device for shooting star orbit videos |
| CN104092948A (en) * | 2014-07-29 | 2014-10-08 | 小米科技有限责任公司 | Method and device for processing image |
| CN104104872A (en) * | 2014-07-16 | 2014-10-15 | 深圳市中兴移动通信有限公司 | Object movement trajectory image synthesis method and device |
| CN104125407A (en) * | 2014-08-13 | 2014-10-29 | 深圳市中兴移动通信有限公司 | Object motion track shooting method and mobile terminal |
| CN104159035A (en) * | 2014-08-22 | 2014-11-19 | 深圳市中兴移动通信有限公司 | Method and device of automatically optimizing orbital shooting effect |
| CN105141840A (en) * | 2015-08-24 | 2015-12-09 | 联想(北京)有限公司 | Information processing method and electronic device |
| CN105554393A (en) * | 2016-01-21 | 2016-05-04 | 努比亚技术有限公司 | Mobile terminal, photographing device and method for photographing pictures |
| CN105607836A (en) * | 2015-12-24 | 2016-05-25 | 深圳市金立通信设备有限公司 | Picture processing method and terminal |
| CN105808051A (en) * | 2016-02-26 | 2016-07-27 | 联想(北京)有限公司 | Image processing method and electronic equipment |
| CN105892753A (en) * | 2016-04-29 | 2016-08-24 | 努比亚技术有限公司 | Method and device for touch screen equipment |
-
2016
- 2016-09-19 CN CN201610832837.1A patent/CN106357979A/en active Pending
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101226113A (en) * | 2008-01-30 | 2008-07-23 | 北京航空航天大学 | Method and apparatus for testing star sensor function based on electric injection star map |
| CN102694967A (en) * | 2011-03-22 | 2012-09-26 | 天津三星光电子有限公司 | A star gazing-realizing method and a device thereof |
| CN102759348A (en) * | 2012-07-18 | 2012-10-31 | 宁波舜宇电子有限公司 | System for automatically identifying coordinates of shooting sites by using star-field digital photography |
| CN103905730A (en) * | 2014-03-24 | 2014-07-02 | 深圳市中兴移动通信有限公司 | Shooting method of mobile terminal and mobile terminal |
| CN104079833A (en) * | 2014-07-02 | 2014-10-01 | 深圳市中兴移动通信有限公司 | Method and device for shooting star orbit videos |
| CN104104872A (en) * | 2014-07-16 | 2014-10-15 | 深圳市中兴移动通信有限公司 | Object movement trajectory image synthesis method and device |
| CN104092948A (en) * | 2014-07-29 | 2014-10-08 | 小米科技有限责任公司 | Method and device for processing image |
| CN104125407A (en) * | 2014-08-13 | 2014-10-29 | 深圳市中兴移动通信有限公司 | Object motion track shooting method and mobile terminal |
| CN104159035A (en) * | 2014-08-22 | 2014-11-19 | 深圳市中兴移动通信有限公司 | Method and device of automatically optimizing orbital shooting effect |
| CN105141840A (en) * | 2015-08-24 | 2015-12-09 | 联想(北京)有限公司 | Information processing method and electronic device |
| CN105607836A (en) * | 2015-12-24 | 2016-05-25 | 深圳市金立通信设备有限公司 | Picture processing method and terminal |
| CN105554393A (en) * | 2016-01-21 | 2016-05-04 | 努比亚技术有限公司 | Mobile terminal, photographing device and method for photographing pictures |
| CN105808051A (en) * | 2016-02-26 | 2016-07-27 | 联想(北京)有限公司 | Image processing method and electronic equipment |
| CN105892753A (en) * | 2016-04-29 | 2016-08-24 | 努比亚技术有限公司 | Method and device for touch screen equipment |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107071278A (en) * | 2017-03-31 | 2017-08-18 | 努比亚技术有限公司 | Terminal and star orbital shooting method |
| CN110930329A (en) * | 2019-11-20 | 2020-03-27 | 维沃移动通信有限公司 | Starry sky image processing method and device |
| CN110930329B (en) * | 2019-11-20 | 2023-04-21 | 维沃移动通信有限公司 | Star image processing method and device |
| CN111010511A (en) * | 2019-12-12 | 2020-04-14 | 维沃移动通信有限公司 | Panoramic body-separating image shooting method and electronic equipment |
| CN111010511B (en) * | 2019-12-12 | 2021-08-10 | 维沃移动通信有限公司 | Panoramic body-separating image shooting method and electronic equipment |
| CN112351207A (en) * | 2020-10-30 | 2021-02-09 | 维沃移动通信有限公司 | Shooting control method and electronic equipment |
| CN112399078A (en) * | 2020-10-30 | 2021-02-23 | 维沃移动通信有限公司 | Shooting method and device and electronic equipment |
| CN112399078B (en) * | 2020-10-30 | 2022-09-02 | 维沃移动通信有限公司 | Shooting method and device and electronic equipment |
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