WO2018113257A1 - Technical field of method, device and system for acquiring target curved surface - Google Patents

Technical field of method, device and system for acquiring target curved surface Download PDF

Info

Publication number
WO2018113257A1
WO2018113257A1 PCT/CN2017/091951 CN2017091951W WO2018113257A1 WO 2018113257 A1 WO2018113257 A1 WO 2018113257A1 CN 2017091951 W CN2017091951 W CN 2017091951W WO 2018113257 A1 WO2018113257 A1 WO 2018113257A1
Authority
WO
WIPO (PCT)
Prior art keywords
target
curved surface
light source
points
preset
Prior art date
Application number
PCT/CN2017/091951
Other languages
French (fr)
Chinese (zh)
Inventor
刘若鹏
栾琳
许发国
Original Assignee
东莞前沿技术研究院
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 东莞前沿技术研究院 filed Critical 东莞前沿技术研究院
Publication of WO2018113257A1 publication Critical patent/WO2018113257A1/en

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T15/003D [Three Dimensional] image rendering
    • G06T15/005General purpose rendering architectures
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/24Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures
    • G01B11/25Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures by projecting a pattern, e.g. one or more lines, moiré fringes on the object
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T15/003D [Three Dimensional] image rendering
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T17/00Three dimensional [3D] modelling, e.g. data description of 3D objects
    • G06T17/30Polynomial surface description
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T2215/00Indexing scheme for image rendering
    • G06T2215/06Curved planar reformation of 3D line structures

Definitions

  • the present invention relates to the field of airships, and in particular to a method, device and system for acquiring a target curved surface
  • the sub airbag is an indispensable component of the airship.
  • the airbag and the aerodynamic shape of the entire airship capsule are maintained at different temperatures by the charge and discharge of the sub airbag, thereby ensuring the continuous floating capacity of the airship. Therefore, in the design practice of the airship, it is necessary to monitor the state of the sub-airbag. Due to the characteristics of the overall structure of the sub-airbag, it can only be monitored by the non-contact method.
  • the existing monitoring method of the airship sub-airbag is based on the three-dimensional reconstruction method, using a laser three-dimensional scanning method or stereo reconstruction based on binocular stereo vision, and three-dimensional reconstruction is a highly feasible method.
  • the laser three-dimensional scanning method using laser three-dimensional scanning method is too expensive, based on binocular stereoscopic stereo reconstruction, because the binocular camera needs to be pre-calibrated, the calibration difficulty is high, and the complicated airflow in the capsule is difficult to ensure.
  • an effective solution has not been proposed due to the high accuracy of the binocular camera, resulting in low accuracy.
  • Embodiments of the present invention provide a method, apparatus, and system for acquiring a target curved surface, so as to at least solve the problem of monitoring the airbag sub-airbag by using a binocular camera in the prior art, because the binocular camera has high registration difficulty. A technical problem that leads to low accuracy.
  • a method for acquiring a target surface including: collecting an image generated by a light projected on a target surface, the image comprising: a plurality of bright stripes, wherein the light is two presets
  • the emitted light from the light source is arranged from the light stripe of the two preset light sources; the plurality of target points are taken from the bright stripe in the image; the coordinate values of the plurality of target points are obtained, and the coordinate values of the plurality of target points are obtained according to the coordinates of the plurality of target points Get the target surface; according to the target surface
  • the volume of the sub-balloon is fixed.
  • an apparatus for acquiring a target curved surface including: an acquisition module, configured to collect an image generated by a light projected on a target curved surface, where the image includes: a plurality of bright stripes, wherein The light is the outgoing light emitted by the two preset light sources, which are respectively arranged by the bright stripes of the two preset light sources; the first obtaining module is configured to take a plurality of target points from the bright stripes in the image; the second acquiring module And acquiring coordinate values of the plurality of target points, and acquiring the target surface according to the coordinate values of the plurality of target points; and determining a module, configured to determine the volume of the sub-airbag according to the target curved surface.
  • a system for acquiring a target curved surface including: two preset light sources for emitting emitted light; and an image capturing device for collecting the projected light from the target curved surface
  • the resulting image includes: a plurality of bright stripes, the target surface is the surface of the airship sub-balloon; the controller is coupled to the image acquisition device for taking a plurality of target points from the bright stripes in the image; The coordinate value of the target point, the target surface is obtained according to the coordinate values of the plurality of target points; and the volume of the airship sub-airbag is determined according to the target curved surface.
  • an image generated by ray casting on a target curved surface is acquired, a plurality of target points are taken from bright stripes in the image, coordinate values of the plurality of target points are acquired, and according to multiple targets The coordinate value of the point acquires the target surface, and the volume of the sub-bag is determined according to the target surface.
  • FIG. 1 is a flow chart of a method of acquiring a target curved surface according to an embodiment of the present invention
  • FIG. 2 is a schematic diagram showing an alternative preset light source and a camera according to an embodiment of the invention
  • FIG. 3 is a schematic diagram of an image captured by an optional camera according to an embodiment of the invention.
  • FIG. 4 is a schematic diagram of an optional acquisition target point coordinate value according to an embodiment of the invention.
  • FIG. 5 is a schematic structural diagram of an apparatus for acquiring a target curved surface according to an embodiment of the present invention.
  • FIG. 6 is a schematic structural diagram of a system for acquiring a target curved surface according to an embodiment of the present invention.
  • an embodiment of a method of acquiring a target curved surface is provided. It is noted that the steps illustrated in the flowchart of the accompanying drawings may be performed in a computer system such as a set of computer executable instructions. And, although the logical order is shown in the flowcharts, in some cases, the steps shown or described may be performed in a different order than the ones described herein.
  • FIG. 1 is a flowchart of a method for acquiring a target curved surface according to an embodiment of the present invention. As shown in FIG. 1, the method includes the following steps:
  • Step S102 collecting an image generated by the light being projected on the target curved surface, the image comprising: a plurality of bright stripes, wherein the light is the outgoing light emitted by the two preset light sources, respectively, from the brightness of the two preset light sources.
  • the stripes are arranged at intervals.
  • the target curved surface is a surface of a sub airbag of an airship to be monitored, and in the foregoing step, The image containing the bright stripes is captured by the camera.
  • the bright stripe may be obtained by splitting and modulating the outgoing light of the preset light source, and the light emitted by the preset light source is split and modulated to obtain a bright and dark line arranged at intervals.
  • the bright and dark lines arranged at intervals will form bright stripes on the surface of the sub-balloon, and then the camera will capture an image of bright stripes.
  • Step S104 taking a plurality of target points from the bright stripes in the image.
  • the above target point is used to determine a target curved surface.
  • the spacing of the plurality of bright stripes is different, and the intensity of the target points is different. Therefore, the monitoring precision of the same target surface is also affected by the spacing of the plurality of bright stripes and the denseness of the target points. The extent of the impact. In the case where there are many target points obtained, the target surface obtained by the monitoring is more accurate, but the calculation amount is larger because there are more target points; and the target surface obtained by monitoring is not enough when the target points are small. Accurate, but the amount of data calculation is small. Therefore, the target point can be obtained according to the actual monitoring requirements to achieve a balance between accuracy and calculation.
  • Step S106 Acquire coordinate values of the plurality of target points, and acquire the target surface according to the coordinate values of the plurality of target points.
  • the coordinate value of the plurality of target points may be combined, and the target surface with higher similarity may be obtained by the three-dimensional reconstruction method, and the obtained result may include a surface for representing the target surface.
  • the method for obtaining a target curved surface provided by the foregoing embodiment has better environmental adaptability, simple system construction, clear image processing, and low cost. It can be applied to the airbag sub-airbag monitoring, and can also be applied to the production of dual-filler stereo imaging cameras and 3D reconstruction applications in darkroom environments. It can play the role of three-dimensional reconstruction, stereo photography, target position monitoring, and stereoscopic image reconstruction in these scenes.
  • the above steps of the present application collect an image generated by ray casting on a target curved surface, take a plurality of target points from the bright stripes in the image, and coordinate values of the plurality of target points, and according to the plurality of The coordinate value of the target point gets the target surface.
  • the above scheme has strong applicability, and even if the preset light source and the posture of the camera change greatly during use, there is no need to calibrate, which is suitable for obtaining variable surface in various scenes, and is particularly suitable for monitoring the airbag in the airbag.
  • the surface of the capsule surface, the accuracy of monitoring can also meet the actual Demand.
  • the method before the image generated by the light being projected on the target curved surface is collected in step 102, the method further includes: Step S108, generating a light stripe, wherein the step of generating the light stripe Includes:
  • Step S112 two preset light sources spaced apart by a preset distance are disposed in front of the target curved surface.
  • Step S114 splitting and modulating the outgoing light of the two preset light sources to form a plurality of bright stripes.
  • the preset light source may be a near-infrared light source, and a plurality of bright stripes are formed by splitting modulation.
  • the preset light source is a near-infrared light source.
  • the first light source 1 emits the first light source splitting light 201
  • the second light source 2 emits the second light source splitting light 20 2
  • the first light source splitting light 201 and the second light splitting light 202 are
  • the target curved surface 203 has a certain overlapping coverage surface
  • the camera 3 for acquiring an image is located between the first light source 1 and the second light source 2, and collects bright stripes formed by the emitted light.
  • the bright stripes emitted by the first light source 1 and the second light source 2 are spaced apart.
  • the distribution position of the camera and the preset light source is not necessarily limited to the above embodiment, and the distance between the first light source 1 and the second light source 2 is known, and the first light source 1 and In the case where the angle between the two bright stripes and the baseline (the line between the first light source 1 and the second light source 2) is reached, the coordinate value of the target point can be acquired by a predetermined calculation method.
  • the diffractive grating may be utilized to form the exiting ray into a plurality of bright stripes.
  • two preset light sources spaced apart by a predetermined distance are disposed in front of the target curved surface, and the emitted light of the two preset light sources is split-modulated, so that the outgoing light forms bright stripes.
  • the above scheme forms an image for acquiring a target point by setting a light source in front of the target surface and splitting the preset light source.
  • taking multiple target points from the bright stripes in the image includes:
  • Step S1041 Take an equally spaced line of the acquired image, where the straight line intersects the plurality of bright stripes.
  • the device used for acquiring the image may be the camera 3, as an optional embodiment,
  • the straight line may be perpendicular to the bright stripe. In the case where the plurality of bright stripe are vertical bright stripe, the straight line is a horizontal line.
  • the camera 3 may be disposed on the first light source 1 and the second light source 2. And the distance from the first light source 1 and the second light source 2 is equal.
  • FIG. 3 is a schematic diagram of an image captured by the optional camera 3 according to an embodiment of the present invention. The result of taking the equally spaced horizontal lines of the acquired image may be as shown in FIG. 3. In an optional embodiment, in combination with the example shown in FIG.
  • the bright stripes formed by the light source 1 and the light source 2 on the target curved surface are vertical bright stripes, at the light source 1 and the light source 2 Equally spaced horizontal lines on the target surface covered by the bright stripes.
  • the equidistant horizontal lines are parallel to the lines connecting the first light source 1 and the second light source 2.
  • Step S1043 Determine an intersection of the straight line and the plurality of bright stripes as a plurality of target points.
  • intersections which are the target points.
  • the above steps of the present application acquire target points by taking equally spaced horizontal lines on the acquired images.
  • the two preset light sources are the first light source and the second light source 2, and the method for acquiring coordinate values of the plurality of target points includes:
  • Step S1061 the two preset light sources are the first light source 1 and the second light source 2, and the first light source 1 of the two preset light sources is determined as the origin, and the connection between the first light source 1 and the second light source 2 is taken as the first Determining, in a dimension, a direction perpendicular to the first dimension on the preset plane is a second dimension, wherein the preset plane is a plane determined by two preset light sources and a target point C to be measured, and the target point C belongs to the second dimension The point on the mth bright strip that is emitted by the source 2 and formed on the target surface.
  • Step S1062 Establish a coordinate system according to the first dimension and the second dimension.
  • FIG. 4 is a schematic diagram of an optional acquisition target coordinate value according to an embodiment of the present invention, and the coordinate system established in the example is combined with the example shown in FIG.
  • the origin 0 is the position of the first light source 1
  • P (1, 0) is the position of the second light source 2
  • the X-axis direction is the direction in which the first light source 1 extends toward the second light source 2
  • the y-axis direction is the first light source. 1.
  • the direction in which the second light source 2 and the target point C are determined to extend perpendicular to the X-axis direction on the plane, and the y-axis coordinate of the target point C is positive.
  • Step S1063 select, among the two coordinate strips of the two light strips emitted by the first light source 1 adjacent to the opposite sides of the target point C as two first auxiliary points A and B, straight line AC and straight line BC near It seems to be a straight line LI; the auxiliary line passing through the origin 0 and the auxiliary point A is L2, the auxiliary line passing through the origin 0 and the auxiliary point B is L3, and the position of the second light source 2 is P(l, 0) and the auxiliary of the target point C
  • the line L4 intersects the auxiliary lines L2 and L3 at the two second auxiliary points E and D, respectively; and acquires the coordinate values (x2, y2) and (xl, yl) of the two second auxiliary points E and D.
  • Point A and Point B are points on the nth and n+1th bright stripes emitted by the first light source 1
  • point C is a point on the mth bright stripe emitted by the second light source 2
  • n and m are known natural numbers that can be measured, that is, the angles ⁇ , ⁇ , and ⁇ of the auxiliary lines L2, L3, and L4 with the x-axis are measurable. That is, the angles ⁇ , ⁇ , ⁇ are known, and in Fig. 4, the distance between the first light source 1 and the second light source 2, that is, the line segment 0 ⁇ is also known.
  • the coordinate value (xl, yl) of the point D can be calculated.
  • the coordinate value of the point E can be calculated (x2 , y2).
  • Step S1065 Acquire coordinate values of the target point according to the coordinate values of the two second auxiliary points E and D and the proportional relationship between the distances of the two first auxiliary points A and B and C.
  • the ratio of the length of the line segment AC to BC can be measured by the bright stripe image as shown in FIG. 2 taken by the camera 3: point C is a point on a known bright stripe in FIG. 3, measurement and point C
  • the distance between the two bright stripes adjacent to the two sides and the bright stripes at the C point, that is, the number of pixels in the horizontal direction between the bright stripes is calculated, and the ratio of the lengths of the segments AC and BC can be obtained.
  • the ratio of the length of the line segment EC to DC can be approximately equal to the ratio of the lengths of the line segments AC and BC, that is, Point 1), the coordinates of point E, and the ratio of EC/DC, the coordinate value of the target point C is obtained.
  • the above steps of the present application achieve the technical purpose of acquiring a target point by constructing a coordinate system and an auxiliary point.
  • Step S1066 Replace the target point C to be replaced with another target point, and repeat steps S1061-S1065 until the coordinate values of all the predetermined target points are acquired.
  • the method further includes:
  • Step S110 Determine a volume of the airship sub-airbag to which the target curved surface belongs according to the target curved surface.
  • the volume of the airship sub-airbag is used to characterize the inflation of the sub-bag, so that the fly can be obtained.
  • Step S112 Obtain a preset safety volume range.
  • the preset safety volume range may include a maximum volume and a minimum volume.
  • Step S114 when the volume of the airship sub-airbag is not in the safe volume range, an alarm signal is issued.
  • the volume of the airship sub-airbag is larger than the maximum volume or smaller than the minimum volume, it is confirmed that the volume of the airbag sub-airbag is not within the safe volume range, and therefore the sub-bag is in an unsafe state, and an alarm signal is issued. It is also possible to have a real data display device for displaying the volume of the sub-bag.
  • the airbag sub-airbag is filled with air inside, is inside the airship main airbag, and is filled with helium gas, and the airship is provided with buoyancy through the helium between the main airbag and the sub-airbag.
  • the airship main airbag may be considered to be too large, possibly due to excessive gas temperature in the main airbag;
  • the airbag airbag may be considered to be too small, possibly due to the air temperature of the airbag being too low.
  • the above steps of the present application obtain an initial safe volume range, and when the volume of the airship sub-airbag is not in the safe volume range, an alarm signal is issued, and the state of the airship sub-airbag is monitored. Thereby, the monitoring of the flight state of the airship is realized.
  • two preset light sources and devices for acquiring images are disposed in the airbag sub-airbag
  • the method for determining the volume of the airship sub-airbag to which the target curved surface belongs according to the target curved surface includes: : Integrate the surface using the distance from the target point on the surface to the source to obtain the internal volume of the airship sub-balloon.
  • 203 is the target curved surface of the airship sub-balloon, that is, the portion photographed by the camera, the first light source 1 and the second light source 2 are both
  • the airbag sub-airbag after the target curved surface is acquired, the vertebral body with the first light source 1 as the cone top and the curved surface 203 as the bottom surface can be obtained, and since the coordinates of each target point on the target curved surface are acquired, it can be known.
  • the distance from each target point on the curved surface 203 to the cone-top light source 1 is integrated with the distance from the target point on the curved surface 203 to the light source 1 to obtain the volume of the vertebral body.
  • the volume of the vertebral body can be obtained by the volume of the vertebral body.
  • the internal volume of the airbag Example 2
  • FIG. 5 is a schematic structural diagram of an apparatus for acquiring a target curved surface according to an embodiment of the present invention. Includes:
  • the acquisition module 50 is configured to collect an image generated by the light being projected on the target curved surface, where the image includes: a plurality of bright stripes, wherein the light is the outgoing light emitted by the two preset light sources, respectively, from the two presets.
  • the light strips of the light source are arranged at intervals.
  • the target curved surface is a surface of a sub-balloon to be monitored, and in the above step, an image containing a plurality of bright stripes may be collected by a camera.
  • the bright stripe may be obtained by splitting and modulating the outgoing light of the preset light source, and the light emitted by the preset light source is split and modulated to obtain bright and dark lines arranged at intervals.
  • the bright and dark lines arranged at intervals will avoid the formation of multiple bright stripes in the sub-balloon, and then the camera will capture images of multiple bright stripes.
  • the target point is used to determine a target curved surface.
  • the spacing of the bright stripes is different, and the density of the target points is not necessarily the same. Therefore, the monitoring accuracy of the same target surface is also affected by the spacing of multiple bright stripes and the concentration of the target points.
  • the degree of influence in the case of more target points obtained, the target surface obtained by the monitoring is more accurate, but the calculation amount is larger due to more target points, and the monitoring result is obtained when the target points are small.
  • the target surface is not precise enough, but the amount of data calculation is small, so the target point can be obtained according to the actual monitoring requirements.
  • the first obtaining module 52 is configured to take a plurality of target points from the bright stripes in the image.
  • the second obtaining module 54 is configured to acquire coordinate values of the plurality of target points, and acquire the target curved surface according to the coordinate values of the plurality of target points.
  • the light source is a preset light source
  • the distance between the light source and the target curved surface is known, and after determining the target point, each target can be calculated according to the distance relationship between the light source and the target curved surface.
  • the coordinate value of the point, in an optional embodiment, the target surface with higher similarity can be directly obtained according to the three-dimensional reconstruction method.
  • the three-dimensional stereo reconstruction method in this embodiment may be the method as described in steps S1061-S1066 in Embodiment 1.
  • a determining module configured to determine a volume of the sub-airbag according to the target curved surface.
  • the method for obtaining a target curved surface provided by the above embodiment is applicable to the environment adaptability, the system is simple to construct, the image processing is clear, and the cost is low.
  • it can also be used to make dual-filler stereo imaging cameras and 3D reconstruction applications in darkroom environments. It can play the role of 3D reconstruction, stereo photography, target position monitoring, and stereo imaging reconstruction in these scenes.
  • the foregoing device of the present application collects an image generated by the light being projected on the target curved surface by the acquiring module, and adopts the first acquiring module to take a plurality of target points from the bright stripes in the image, and adopts the second acquiring module.
  • Obtain coordinate values of multiple target points and obtain a target surface according to coordinate values of the plurality of target points, and determine a volume of the sub-airbag according to the target curved surface by the determining module.
  • the above scheme has strong applicability, and even if the attitude of the light source and the camera changes greatly during use, calibration is not required, and the condition of the sub-balloon can be effectively monitored, and the accuracy of the monitoring can also meet the actual demand.
  • the foregoing apparatus further includes: a generating module, configured to generate a bright stripe before acquiring an image generated by the ray being projected on the target curved surface, where the generating module includes
  • a setting unit configured to set two preset light sources spaced apart by a preset distance in front of the target curved surface.
  • a modulating unit configured to perform beam splitting modulation on the outgoing light of the two preset light sources, so that the outgoing light forms a bright stripe.
  • the above-mentioned device of the present application sets two preset light sources spaced apart by a preset distance in front of the target curved surface by the setting unit, and splits and modulates the emitted light of the two preset light sources through the modulating unit to make the outgoing light.
  • the above scheme forms an image for acquiring a target point by setting a light source in front of the target curved surface and splitting the light source.
  • the first obtaining module 52 includes:
  • the first acquiring unit is configured to take an equally spaced line of the captured image, where the straight line intersects the bright stripe.
  • the first determining unit is configured to determine that an intersection of the straight line and the bright stripe is a plurality of target points.
  • the second obtaining module 54 includes:
  • the second determining unit is configured to determine that the first light source 1 of the two preset light sources is an origin, and the connection between the first light source 1 and the second light source 2 is used as a first dimension, and is determined in a preset plane. Vertically perpendicular to the first dimension The direction is a second dimension, where the preset plane is a plane determined by the two preset light sources and a target point to be tested, and the target point to be tested corresponds to the second light source 2 a bright stripe, the target point to be measured corresponds to a bright stripe emitted by the second light source 2.
  • an establishing unit configured to establish a coordinate system according to the first dimension and the second dimension
  • a second acquiring unit configured to select, in the coordinate system, a bright point among two bright stripes emitted by the first light source 1 adjacent to the two sides of the target point as the two first auxiliary points, and the second light source 2 and The intersection of the line connecting the target point and the two auxiliary lines is two second auxiliary points, wherein the two auxiliary lines are the connection between the first light source 1 and the first auxiliary point;
  • the third obtaining unit is configured to acquire a coordinate value of the target point according to a coordinate value of the second auxiliary point and a ratio of the distance of the first auxiliary point.
  • the foregoing apparatus further includes:
  • a determining module configured to determine, according to the target curved surface, a volume of the airship sub-airbag to which the target curved surface belongs;
  • a third obtaining module configured to acquire a preset safety volume range
  • the alarm module is configured to issue an alarm signal when the volume of the airship sub-airbag is not within a safe volume range.
  • FIG. 6 is a schematic structural diagram of a system for acquiring a target curved surface according to an embodiment of the present invention. Includes:
  • Two preset light sources 60 for emitting outgoing light are provided.
  • the target curved surface is a surface of a sub-balloon to be monitored, and in the above step, an image containing a plurality of bright stripes may be collected by a camera.
  • the plurality of bright stripes may be obtained by splitting and modulating the outgoing light of the light source, and the light emitted by the light source is split and modulated to obtain bright and dark lines arranged at intervals.
  • the bright and dark lines will avoid multiple bright stripes in the sub-balloon, and then use the camera to capture the image of the bright stripes.
  • the image capturing device 62 is configured to collect an image generated by the projected light being projected on the target curved surface, and the image includes: a bright stripe, and the target curved surface is a surface of the sub-balloon. [0098] Specifically, the target point is used to determine a target curved surface.
  • the spacing of the bright stripes is different, and the density of the target points is not necessarily the same, so the monitoring accuracy of the same target surface is also affected by the spacing of the bright stripes and the density of the target points. Influence, in the case where there are many target points obtained, the target surface obtained by the monitoring is more accurate, but the calculation amount is larger due to more target points, and the target surface is monitored when the target points are small. Not precise enough, but the amount of data calculation is small, so you can get the target point according to the actual monitoring requirements.
  • the processor 64 is connected to the image capturing device, and is configured to take a plurality of target points from the bright stripes in the image; acquire coordinate values of the plurality of target points, and obtain a target surface according to the coordinate values of the plurality of target points; The volume of the sub-bag is determined according to the target surface.
  • the light source is a preset light source
  • the distance between the light source and the target curved surface is known.
  • the coordinate value of each target point can be calculated according to the distance relationship between the light source and the target surface.
  • the similarity can be directly obtained according to the three-dimensional reconstruction method. High target surface.
  • the method for obtaining a target curved surface provided by the above embodiment is applicable to the environment adaptability, the system is simple to construct, the image processing is clear, and the cost is low.
  • it can also be used to make dual-filler stereo imaging cameras and 3D reconstruction applications in darkroom environments. It can play the role of 3D reconstruction, stereo photography, target position monitoring, and stereo imaging reconstruction in these scenes.
  • the above-mentioned system of the present application collects an image generated by the emitted light on the target curved surface through an image capturing device by using the emitted light emitted by the preset light source, and is connected to the image collecting device through the processor, from the image.
  • the plurality of target points are taken on the bright stripe; the coordinate values of the plurality of target points are obtained, the target surface is obtained according to the coordinate values of the plurality of target points; and the volume of the sub-bag is determined according to the target surface.
  • the above-mentioned scheme has strong applicability. Even if the attitude of the light source and the camera changes greatly during use, there is no need to calibrate, and the condition of the sub-balloon can be effectively monitored, and the accuracy of the monitoring can also meet the actual demand.
  • the system further includes: the preset light source is two light sources disposed in front of the target curved surface and spaced apart from the target curved surface by a predetermined distance.
  • the light source is a near-infrared light source placed in front of the target curved surface, and the emitted light of the two light sources has a certain repeated coverage on the target curved surface, and the camera for acquiring images is located at two. Between the near-infrared light sources, a plurality of bright stripes formed by the emitted light of the near-infrared light source.
  • the distribution position of the camera and the light source is not necessarily limited to the above embodiment, and the distance between the two light sources and the disposal distance between the two light sources and the target curved surface are known. , you can get the coordinates of the target point.
  • the disclosed technical content may be implemented in other manners.
  • the device embodiments described above are only schematic.
  • the division of the unit may be a logical function division.
  • the actual implementation may have another division manner.
  • multiple units or components may be combined or may be Integration into another system, or some features can be ignored, or not executed.
  • the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, unit or module, and may be electrical or otherwise.
  • the unit described as a separate component may or may not be physically distributed, and the component displayed as a unit may or may not be a physical unit, that is, may be located in one place, or may be distributed to multiple On the unit. Some or all of the units may be selected according to actual needs to achieve the objectives of the embodiment of the present embodiment.
  • each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
  • the above integrated unit can be implemented in the form of hardware or in the form of a software functional unit.
  • the integrated unit if implemented in the form of a software functional unit and sold or used as a standalone product, may be stored in a computer readable storage medium.
  • the technical solution of the present invention may contribute to the prior art or all or part of the technical solution may be embodied in the form of a software product stored in a storage medium.
  • a number of instructions are included to cause a computer device (which may be a personal computer, server or network device, etc.) to perform all or part of the steps of the methods described in various embodiments of the present invention.
  • the foregoing storage medium includes: a USB flash drive, a read only memory (ROM, Read-Only)
  • RAM Random Access Memory
  • removable hard disk disk or optical disk, and other media that can store program code.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Computer Graphics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Physics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Geometry (AREA)
  • Software Systems (AREA)
  • Algebra (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Length Measuring Devices By Optical Means (AREA)

Abstract

Provided are a method, device and system for acquiring a target curved surface. The method comprises: collecting an image generated by a light ray projected onto a target curved surface, the image comprising: a plurality of bright stripes, wherein the light ray is an emergent light ray emitted from two pre-set light sources, and the bright stripes respectively from the two pre-set light sources are arranged at intervals; obtaining a plurality of target points from the bright stripes in the image; acquiring a coordinate value of the plurality of target points, and according to the coordinate value of the plurality of target points, acquiring the target curved surface; and according to the target curved surface, determining the volume of a ballonet. The technical problem in the prior art that when a binocular camera is used to monitor the state of an airship ballonet, high registration difficulty of the binocular camera results in low accuracy is solved.

Description

说明书 发明名称:获取目标曲面的方法、 装置和系统技术领域  Description: Method, device and system for obtaining a target curved surface
[0001] 本发明涉及飞艇领域, 具体而言, 涉及一种获取目标曲面的方法、 装置和系统 背景技术  [0001] The present invention relates to the field of airships, and in particular to a method, device and system for acquiring a target curved surface
[0002] 副气囊是飞艇必不可少的组成部分, 通过副气囊的充放气实现在不同气温下整 个飞艇囊体的气压和气动外形的保持, 从而保障飞艇的长吋间持续浮空能力, 因此在飞艇的设计实践中, 吋刻监控副气囊的状态是必要的, 由于副气囊整体 结构的特性, 只能用非接触方法进行监测。  [0002] The sub airbag is an indispensable component of the airship. The airbag and the aerodynamic shape of the entire airship capsule are maintained at different temperatures by the charge and discharge of the sub airbag, thereby ensuring the continuous floating capacity of the airship. Therefore, in the design practice of the airship, it is necessary to monitor the state of the sub-airbag. Due to the characteristics of the overall structure of the sub-airbag, it can only be monitored by the non-contact method.
技术问题  technical problem
[0003] 现有的飞艇副气囊的监控方法是在三维重构方法的基础上, 采用激光三维扫描 方法或基于双目立体视觉的立体重构, 三维重构是一项可行性很高的方法, 但 采用激光三维扫描方法的激光三维扫描成本太高, 基于双目立体视觉的立体重 构吋, 由于双目摄像机需要预先校准好, 校准难度较高, 并且囊内复杂的气流 等情况难以保证双目视觉所必须的稳定状态, 因此立体视觉在超过 25m左右的距 离上精度不能达标。 针对现有技术中在采用双目摄像机监控飞艇副气囊的状态 吋, 由于双目摄像机的配准难度高导致精确度低的问题, 目前尚未提出有效的 解决方案。  [0003] The existing monitoring method of the airship sub-airbag is based on the three-dimensional reconstruction method, using a laser three-dimensional scanning method or stereo reconstruction based on binocular stereo vision, and three-dimensional reconstruction is a highly feasible method. However, the laser three-dimensional scanning method using laser three-dimensional scanning method is too expensive, based on binocular stereoscopic stereo reconstruction, because the binocular camera needs to be pre-calibrated, the calibration difficulty is high, and the complicated airflow in the capsule is difficult to ensure. The steady state necessary for binocular vision, so stereoscopic vision cannot reach the standard at a distance of more than 25m. In view of the state of the art in monitoring the airbag sub-airbag by using a binocular camera in the prior art, an effective solution has not been proposed due to the high accuracy of the binocular camera, resulting in low accuracy.
问题的解决方案  Problem solution
技术解决方案  Technical solution
[0004] 本发明实施例提供了一种获取目标曲面的方法、 装置和系统, 以至少解决现有 技术中在采用双目摄像机监控飞艇副气囊的状态吋, 由于双目摄像机的配准难 度高导致精确度低的技术问题。 根据本发明实施例的一个方面, 提供了一种获 取目标曲面的方法, 包括: 采集由光线投射在目标曲面上而产生的图像, 图像 包括: 多个亮条纹, 其中, 光线为两台预设光源发出的出射光线, 分别来自两 台预设光源的亮条纹间隔排列; 从图像中的亮条纹上取多个目标点; 获取多个 目标点的坐标值, 并根据多个目标点的坐标值获取目标曲面; 根据目标曲面确 定副气囊的容积。 根据本发明实施例的另一方面, 还提供了一种获取目标曲面 的装置, 包括: 采集模块, 用于采集由光线投射在目标曲面上而产生的图像, 图像包括: 多个亮条纹, 其中, 光线为两台预设光源发出的出射光线, 分别来 自两台预设光源的亮条纹间隔排列; 第一获取模块, 用于从图像中的亮条纹上 取多个目标点; 第二获取模块, 用于获取多个目标点的坐标值, 并根据多个目 标点的坐标值获取目标曲面; 确定模块, 用于根据目标曲面确定副气囊的容积 。 根据本发明实施例的又一方面, 还提供了一种获取目标曲面的系统, 包括: 两台预设光源, 用于发出的出射光线; 图像采集设备, 用于采集由出射光线投 射在目标曲面上而产生的图像, 图像包括: 多个亮条纹, 目标曲面为飞艇副气 囊的表面; 控制器, 与图像采集设备相连, 用于从图像中的亮条纹上取多个目 标点; 获取多个目标点的坐标值, 根据多个目标点的坐标值获取目标曲面; 并 根据目标曲面确定飞艇副气囊的容积。 。 Embodiments of the present invention provide a method, apparatus, and system for acquiring a target curved surface, so as to at least solve the problem of monitoring the airbag sub-airbag by using a binocular camera in the prior art, because the binocular camera has high registration difficulty. A technical problem that leads to low accuracy. According to an aspect of the embodiments of the present invention, a method for acquiring a target surface is provided, including: collecting an image generated by a light projected on a target surface, the image comprising: a plurality of bright stripes, wherein the light is two presets The emitted light from the light source is arranged from the light stripe of the two preset light sources; the plurality of target points are taken from the bright stripe in the image; the coordinate values of the plurality of target points are obtained, and the coordinate values of the plurality of target points are obtained according to the coordinates of the plurality of target points Get the target surface; according to the target surface The volume of the sub-balloon is fixed. According to another aspect of the embodiments of the present invention, an apparatus for acquiring a target curved surface is further provided, including: an acquisition module, configured to collect an image generated by a light projected on a target curved surface, where the image includes: a plurality of bright stripes, wherein The light is the outgoing light emitted by the two preset light sources, which are respectively arranged by the bright stripes of the two preset light sources; the first obtaining module is configured to take a plurality of target points from the bright stripes in the image; the second acquiring module And acquiring coordinate values of the plurality of target points, and acquiring the target surface according to the coordinate values of the plurality of target points; and determining a module, configured to determine the volume of the sub-airbag according to the target curved surface. According to still another aspect of the embodiments of the present invention, a system for acquiring a target curved surface is provided, including: two preset light sources for emitting emitted light; and an image capturing device for collecting the projected light from the target curved surface The resulting image includes: a plurality of bright stripes, the target surface is the surface of the airship sub-balloon; the controller is coupled to the image acquisition device for taking a plurality of target points from the bright stripes in the image; The coordinate value of the target point, the target surface is obtained according to the coordinate values of the plurality of target points; and the volume of the airship sub-airbag is determined according to the target curved surface. .
发明的有益效果  Advantageous effects of the invention
有益效果  Beneficial effect
[0005] 在本发明实施例中, 采集由光线投射在目标曲面上而产生的图像, 从图像中的 亮条纹上取多个目标点, 获取多个目标点的坐标值, 并根据多个目标点的坐标 值获取目标曲面, 并根据目标曲面确定副气囊的容积。 上述方案环境适用性强 , 使用过程中即使光源和相机的姿态发生较大的变化, 也无需校准, 并可以有 效的监测出副气囊的状况, 监测的精度也能满足实际需求。  [0005] In the embodiment of the present invention, an image generated by ray casting on a target curved surface is acquired, a plurality of target points are taken from bright stripes in the image, coordinate values of the plurality of target points are acquired, and according to multiple targets The coordinate value of the point acquires the target surface, and the volume of the sub-bag is determined according to the target surface. The above scheme has strong applicability. Even if the attitude of the light source and the camera changes greatly during the use, there is no need to calibrate, and the condition of the sub-balloon can be effectively monitored, and the accuracy of the monitoring can also meet the actual demand.
对附图的简要说明  Brief description of the drawing
附图说明  DRAWINGS
[0006] 此处所说明的附图用来提供对本发明的进一步理解, 构成本申请的一部分, 本 发明的示意性实施例及其说明用于解释本发明, 并不构成对本发明的不当限定 。 在附图中:  The drawings are intended to provide a further understanding of the present invention, and are intended to be a part of the present invention, and the description of the present invention and the description thereof are not intended to limit the invention. In the drawing:
[0007] 图 1是根据本发明实施例的一种获取目标曲面的方法的流程图;  1 is a flow chart of a method of acquiring a target curved surface according to an embodiment of the present invention;
[0008] 图 2是根据本发明实施例的一种可选的预设光源和相机的分布示意图; 2 is a schematic diagram showing an alternative preset light source and a camera according to an embodiment of the invention;
[0009] 图 3是根据本发明实施例的一种可选的相机采集到的图像示意图; 3 is a schematic diagram of an image captured by an optional camera according to an embodiment of the invention;
[0010] 图 4是根据本发明实施例的一种可选的获取目标点坐标值的示意图; [0011] 图 5是根据本发明实施例的一种获取目标曲面的装置的结构示意图; 以及 4 is a schematic diagram of an optional acquisition target point coordinate value according to an embodiment of the invention; [0011] FIG. 5 is a schematic structural diagram of an apparatus for acquiring a target curved surface according to an embodiment of the present invention;
[0012] 图 6是根据本发明实施例的一种获取目标曲面的系统的结构示意图。 6 is a schematic structural diagram of a system for acquiring a target curved surface according to an embodiment of the present invention.
本发明的实施方式 Embodiments of the invention
[0013] 为了使本技术领域的人员更好地理解本发明方案, 下面将结合本发明实施例中 的附图, 对本发明实施例中的技术方案进行清楚、 完整地描述, 显然, 所描述 的实施例仅仅是本发明一部分的实施例, 而不是全部的实施例。 基于本发明中 的实施例, 本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其 他实施例, 都应当属于本发明保护的范围。  The technical solutions in the embodiments of the present invention will be clearly and completely described in the following with reference to the accompanying drawings in the embodiments of the present invention. The embodiments are merely a part of the embodiments of the invention, and not all of the embodiments. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without departing from the inventive scope should fall within the scope of the present invention.
[0014] 需要说明的是, 本发明的说明书和权利要求书及上述附图中的术语"第一"、 " 第二"等是用于区别类似的对象, 而不必用于描述特定的顺序或先后次序。 应该 理解这样使用的数据在适当情况下可以互换, 以便这里描述的本发明的实施例 能够以除了在这里图示或描述的那些以外的顺序实施。 此外, 术语"包括"和"具 有"以及他们的任何变形, 意图在于覆盖不排他的包含, 例如, 包含了一系列步 骤或单元的过程、 方法、 系统、 产品或设备不必限于清楚地列出的那些步骤或 单元, 而是可包括没有清楚地列出的或对于这些过程、 方法、 产品或设备固有 的其它步骤或单元。  [0014] It should be noted that the terms "first", "second" and the like in the specification and claims of the present invention and the above drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or Prioritization. It is to be understood that the data so used may be interchanged as appropriate, so that the embodiments of the invention described herein can be implemented in a sequence other than those illustrated or described herein. In addition, the terms "comprises" and "comprising" and "comprises" and "the" are intended to cover a non-exclusive inclusion, for example, a process, method, system, product, or device that comprises a series of steps or units is not necessarily limited to Those steps or units may include other steps or units not explicitly listed or inherent to such processes, methods, products or devices.
[0015] 实施例 1  [0015] Example 1
[0016] 根据本发明实施例, 提供了一种获取目标曲面的方法实施例, 需要说明的是, 在附图的流程图示出的步骤可以在诸如一组计算机可执行指令的计算机系统中 执行, 并且, 虽然在流程图中示出了逻辑顺序, 但是在某些情况下, 可以以不 同于此处的顺序执行所示出或描述的步骤。  [0016] In accordance with an embodiment of the present invention, an embodiment of a method of acquiring a target curved surface is provided. It is noted that the steps illustrated in the flowchart of the accompanying drawings may be performed in a computer system such as a set of computer executable instructions. And, although the logical order is shown in the flowcharts, in some cases, the steps shown or described may be performed in a different order than the ones described herein.
[0017] 图 1是根据本发明实施例的获取目标曲面的方法的流程图, 如图 1所示, 该方法 包括如下步骤:  1 is a flowchart of a method for acquiring a target curved surface according to an embodiment of the present invention. As shown in FIG. 1, the method includes the following steps:
[0018] 步骤 S102, 采集由光线投射在目标曲面上而产生的图像, 图像包括: 多个亮条 纹, 其中, 光线为两台预设光源发出的出射光线, 分别来自两台预设光源的亮 条纹间隔排列。  [0018] Step S102, collecting an image generated by the light being projected on the target curved surface, the image comprising: a plurality of bright stripes, wherein the light is the outgoing light emitted by the two preset light sources, respectively, from the brightness of the two preset light sources. The stripes are arranged at intervals.
[0019] 具体的, 上述目标曲面为需要监测的飞艇的副气囊的表面, 在上述步骤中, 可 以由相机来采集含有亮条纹的图像。 [0019] Specifically, the target curved surface is a surface of a sub airbag of an airship to be monitored, and in the foregoing step, The image containing the bright stripes is captured by the camera.
[0020] 在一种可选的实施例中, 上述亮条纹可以是对预设光源的出射光线进行分束调 制得到, 由于预设光源的出射光线经过分束调制会得到间隔排列的亮暗线, 间 隔排列的亮暗线会在副气囊表面构成亮条纹, 再采用相机采集亮条纹构成的图 像。  [0020] In an optional embodiment, the bright stripe may be obtained by splitting and modulating the outgoing light of the preset light source, and the light emitted by the preset light source is split and modulated to obtain a bright and dark line arranged at intervals. The bright and dark lines arranged at intervals will form bright stripes on the surface of the sub-balloon, and then the camera will capture an image of bright stripes.
[0021] 步骤 S104, 从图像中的亮条纹上取多个目标点。  [0021] Step S104, taking a plurality of target points from the bright stripes in the image.
[0022] 具体的, 上述目标点用于确定目标曲面。 [0022] Specifically, the above target point is used to determine a target curved surface.
[0023] 此处需要说明的是, 多个亮条纹的间距不同, 取目标点的密集程度也不同, 因 此同一个目标曲面的监测精度也会受到多个亮条纹的间距以及取目标点的密集 程度的影响。 在取得的目标点较多的情况下, 监测得到的目标曲面更精确, 但 由于目标点较多, 计算量也较大; 而在取得的目标点较少的情况下, 监测得到 的目标曲面不够精确, 但数据计算量较小。 因此可以根据实际的监测要求来取 得目标点, 以达到精确度与计算量之间的平衡。  [0023] It should be noted that the spacing of the plurality of bright stripes is different, and the intensity of the target points is different. Therefore, the monitoring precision of the same target surface is also affected by the spacing of the plurality of bright stripes and the denseness of the target points. The extent of the impact. In the case where there are many target points obtained, the target surface obtained by the monitoring is more accurate, but the calculation amount is larger because there are more target points; and the target surface obtained by monitoring is not enough when the target points are small. Accurate, but the amount of data calculation is small. Therefore, the target point can be obtained according to the actual monitoring requirements to achieve a balance between accuracy and calculation.
[0024] 步骤 S106, 获取多个目标点的坐标值, 并根据多个目标点的坐标值获取目标曲 面。  [0024] Step S106: Acquire coordinate values of the plurality of target points, and acquire the target surface according to the coordinate values of the plurality of target points.
[0025] 在上述步骤中, 在确定目标点之后, 可以结合多个目标点的坐标值, 通过三维 立体重构方法得到相似度较高的目标曲面, 得到的结果可以包括用于表示目标 曲面的函数和 /或目标曲面示意图。  [0025] In the above steps, after determining the target point, the coordinate value of the plurality of target points may be combined, and the target surface with higher similarity may be obtained by the three-dimensional reconstruction method, and the obtained result may include a surface for representing the target surface. Schematic diagram of functions and/or target surfaces.
[0026] 此处需要说明的是, 上述实施例提供的获取目标曲面的方法所适用的环境适应 性较好、 系统搭建简单、 图像处理明了、 成本低廉。 可以应用于飞艇副气囊监 控, 还可以应用于制作双补光灯立体成像相机、 暗室环境下的三维重构应用等 。 能够在这些场景中发挥三维重构、 立体拍照、 目标位置监测、 立体成像重构 的作用。  [0026] It should be noted that the method for obtaining a target curved surface provided by the foregoing embodiment has better environmental adaptability, simple system construction, clear image processing, and low cost. It can be applied to the airbag sub-airbag monitoring, and can also be applied to the production of dual-filler stereo imaging cameras and 3D reconstruction applications in darkroom environments. It can play the role of three-dimensional reconstruction, stereo photography, target position monitoring, and stereoscopic image reconstruction in these scenes.
[0027] 由上可知, 本申请上述步骤采集由光线投射在目标曲面上而产生的图像, 从图 像中的亮条纹上取多个目标点, 以及多个目标点的坐标值, 并根据多个目标点 的坐标值获取目标曲面。 上述方案环境适用性强, 使用过程中即使预设光源和 相机的姿态发生较大的变化, 也无需校准, 适用于多种场景下对可变曲面的获 取, 尤其适用于监测飞艇副气囊内的囊体表面曲面, 监测的精度也能满足实际 需求。 [0027] As can be seen from the above, the above steps of the present application collect an image generated by ray casting on a target curved surface, take a plurality of target points from the bright stripes in the image, and coordinate values of the plurality of target points, and according to the plurality of The coordinate value of the target point gets the target surface. The above scheme has strong applicability, and even if the preset light source and the posture of the camera change greatly during use, there is no need to calibrate, which is suitable for obtaining variable surface in various scenes, and is particularly suitable for monitoring the airbag in the airbag. The surface of the capsule surface, the accuracy of monitoring can also meet the actual Demand.
[0028] 可选的, 根据本申请上述实施例, 在步骤 102中采集由光线投射在目标曲面上 而产生的图像之前, 方法还包括: 步骤 S108, 生成亮条纹, 其中, 生成亮条纹 的步骤包括:  [0028] Optionally, according to the foregoing embodiment of the present application, before the image generated by the light being projected on the target curved surface is collected in step 102, the method further includes: Step S108, generating a light stripe, wherein the step of generating the light stripe Includes:
[0029] 步骤 S112, 在目标曲面前方设置间隔预设距离的两台预设光源。  [0029] Step S112, two preset light sources spaced apart by a preset distance are disposed in front of the target curved surface.
[0030] 步骤 S114, 对两台预设光源的出射光线进行分束调制, 使出射光线形成多个亮 条纹。  [0030] Step S114, splitting and modulating the outgoing light of the two preset light sources to form a plurality of bright stripes.
[0031] 具体的, 上述预设光源可以是近红外光源, 通过分束调制后形成多个亮条纹。  [0031] Specifically, the preset light source may be a near-infrared light source, and a plurality of bright stripes are formed by splitting modulation.
[0032] 图 2是根据本发明实施例的一种可选的预设光源和相机的分布示意图, 在一种 可选的情况下, 结合图 2所示的示例, 预设光源为近红外光源, 放置于目标曲面 前, 第一光源 1发出第一光源分束光线 201, 第二光源 2发出第二光源分束光线 20 2, 第一光源分束光线 201和第二光源分束光线 202在目标曲面 203上具有一定的 重叠覆盖面, 用于采集图像的相机 3位于第一光源 1和第二光源 2之间, 采集出射 光线构成的亮条纹。 在目标曲面 203上第一光源分束光线 201和第二光源分束光 线 202的重叠覆盖面上, 所述第一光源 1和第二光源 2发出的亮条纹间隔排列。 2 is a schematic diagram of an optional preset light source and a camera according to an embodiment of the present invention. In an optional case, in combination with the example shown in FIG. 2, the preset light source is a near-infrared light source. Before being placed on the target surface, the first light source 1 emits the first light source splitting light 201, the second light source 2 emits the second light source splitting light 20 2, and the first light source splitting light 201 and the second light splitting light 202 are The target curved surface 203 has a certain overlapping coverage surface, and the camera 3 for acquiring an image is located between the first light source 1 and the second light source 2, and collects bright stripes formed by the emitted light. On the overlapping coverage surfaces of the first source splitting ray 201 and the second source splitting beam 202 on the target curved surface 203, the bright stripes emitted by the first light source 1 and the second light source 2 are spaced apart.
[0033] 此处需要说明的是, 上述相机以及预设光源的分布位置并不一定局限于上述实 施例, 在知晓第一光源 1和第二光源 2之间的距离, 以及第一光源 1和第二光源 2 个亮条纹与基线 (第一光源 1与第二光源 2之间的连线) 之间的夹角的情况下, 通过预定的计算方法就能够获取到目标点的坐标值。 [0033] It should be noted here that the distribution position of the camera and the preset light source is not necessarily limited to the above embodiment, and the distance between the first light source 1 and the second light source 2 is known, and the first light source 1 and In the case where the angle between the two bright stripes and the baseline (the line between the first light source 1 and the second light source 2) is reached, the coordinate value of the target point can be acquired by a predetermined calculation method.
[0034] 在一种可选的实施例中, 可以利用衍射光栅使出射光线形成多个亮条纹。 [0034] In an alternative embodiment, the diffractive grating may be utilized to form the exiting ray into a plurality of bright stripes.
[0035] 由上可知, 本申请上述步骤在目标曲面前方设置间隔预设距离的两台预设光源 , 对两台预设光源的出射光线进行分束调制, 使出射光线形成亮条纹。 上述方 案通过在目标曲面前方设置光源, 并对预设光源进行分束调制, 形成了用于获 取目标点的图像。 [0035] As can be seen from the above, in the above steps of the present application, two preset light sources spaced apart by a predetermined distance are disposed in front of the target curved surface, and the emitted light of the two preset light sources is split-modulated, so that the outgoing light forms bright stripes. The above scheme forms an image for acquiring a target point by setting a light source in front of the target surface and splitting the preset light source.
[0036] 可选的, 根据本申请上述实施例, 步骤 104中, 从图像中的亮条纹上取多个目 标点, 包括:  [0036] Optionally, according to the foregoing embodiment of the present application, in step 104, taking multiple target points from the bright stripes in the image includes:
[0037] 步骤 S1041 , 对采集的图像取等间距直线, 其中, 直线与多个亮条纹相交。  [0037] Step S1041: Take an equally spaced line of the acquired image, where the straight line intersects the plurality of bright stripes.
[0038] 具体的, 上述采集图像所使用的设备可以是相机 3, 作为一种可选的实施例, 上述直线可以与亮条纹垂直, 在多个亮条纹为竖直亮条纹的情况下, 上述直线 为水平线, 结合图 2所示的示例, 相机 3可以部署于第一光源 1和第二光源 2之间 , 且与第一光源 1和第二光源 2的距离相等。 图 3是根据本发明实施例的一种可选 的相机 3采集到的图像示意图, 对采集的图像取等间距水平线的结果可以如图 3 所示。 在一种可选的实施例中, 结合图 3所示的示例, 通过分束调制, 光源 1和 光源 2在目标曲面上形成的亮条纹均为竖直的亮条纹, 在光源 1和光源 2的亮条纹 均覆盖的目标曲面上取等间距水平线。 等间距水平线平行于第一光源 1和第二光 源 2的连线。 [0038] Specifically, the device used for acquiring the image may be the camera 3, as an optional embodiment, The straight line may be perpendicular to the bright stripe. In the case where the plurality of bright stripe are vertical bright stripe, the straight line is a horizontal line. In conjunction with the example shown in FIG. 2, the camera 3 may be disposed on the first light source 1 and the second light source 2. And the distance from the first light source 1 and the second light source 2 is equal. FIG. 3 is a schematic diagram of an image captured by the optional camera 3 according to an embodiment of the present invention. The result of taking the equally spaced horizontal lines of the acquired image may be as shown in FIG. 3. In an optional embodiment, in combination with the example shown in FIG. 3, by the beam splitting modulation, the bright stripes formed by the light source 1 and the light source 2 on the target curved surface are vertical bright stripes, at the light source 1 and the light source 2 Equally spaced horizontal lines on the target surface covered by the bright stripes. The equidistant horizontal lines are parallel to the lines connecting the first light source 1 and the second light source 2.
[0039] 步骤 S1043 , 确定直线与多个亮条纹的交点为多个目标点。  [0039] Step S1043: Determine an intersection of the straight line and the plurality of bright stripes as a plurality of target points.
[0040] 每个水平线与第一光源 1和第二光源 2的亮条纹均产生交点, 这些交点即为目标 点。  [0040] Each horizontal line and the bright strips of the first light source 1 and the second light source 2 generate intersections, which are the target points.
[0041] 由上可知, 本申请上述步骤通过对采集的图像取等间距水平线, 来获取目标点  [0041] As can be seen from the above, the above steps of the present application acquire target points by taking equally spaced horizontal lines on the acquired images.
[0042] 可选的, 根据本申请上述实施例, 在步骤 106中, 所述两台预设光源为第一光 源和第二光源 2, 获取多个目标点的坐标值的方法包括: [0042] Optionally, according to the foregoing embodiment of the present application, in step 106, the two preset light sources are the first light source and the second light source 2, and the method for acquiring coordinate values of the plurality of target points includes:
[0043] 步骤 S1061 , 两台预设光源为第一光源 1和第二光源 2, 确定两台预设光源中第 一光源 1为原点, 第一光源 1与第二光源 2的连线作为第一维度, 确定在预设平面 上与第一维度垂直的方向为第二维度, 其中, 预设平面为由两台预设光源与一 待测目标点 C确定的平面, 目标点 C属于第二光源 2所发出并在目标曲面上形成的 第 m条亮条纹上的点。  [0043] Step S1061, the two preset light sources are the first light source 1 and the second light source 2, and the first light source 1 of the two preset light sources is determined as the origin, and the connection between the first light source 1 and the second light source 2 is taken as the first Determining, in a dimension, a direction perpendicular to the first dimension on the preset plane is a second dimension, wherein the preset plane is a plane determined by two preset light sources and a target point C to be measured, and the target point C belongs to the second dimension The point on the mth bright strip that is emitted by the source 2 and formed on the target surface.
[0044] 步骤 S 1062, 根据第一维度和第二维度建立坐标系。  [0044] Step S1062: Establish a coordinate system according to the first dimension and the second dimension.
[0045] 在一种可选的实施例中, 图 4是根据本发明实施例的一种可选的获取目标点坐 标值的示意图, 结合图 4所示的示例, 该示例中建立的坐标系的原点 0为第一光 源 1的位置, P (1,0) 为第二光源 2的位置, X轴方向为第一光源 1向第二光源 2延 伸的方向, y轴方向为在第一光源 1、 第二光源 2和目标点 C确定的平面上垂直于 X 轴方向延伸的方向, 且目标点 C的 y轴坐标为正。  [0045] In an optional embodiment, FIG. 4 is a schematic diagram of an optional acquisition target coordinate value according to an embodiment of the present invention, and the coordinate system established in the example is combined with the example shown in FIG. The origin 0 is the position of the first light source 1, P (1, 0) is the position of the second light source 2, the X-axis direction is the direction in which the first light source 1 extends toward the second light source 2, and the y-axis direction is the first light source. 1. The direction in which the second light source 2 and the target point C are determined to extend perpendicular to the X-axis direction on the plane, and the y-axis coordinate of the target point C is positive.
[0046] 步骤 S1063 , 如图 4所示, 在坐标系中选取与目标点 C相对两侧相邻的由第一光 源 1发出的两个亮条纹中的亮点作为两个第一辅助点 A和 B, 直线 AC和直线 BC近 似为一条直线 LI ; 经过原点 0和辅助点 A的辅助线为 L2, 经过原点 0和辅助点 B 的辅助线为 L3, 第二光源 2所在位置 P(l, 0)与目标点 C的辅助线 L4与辅助线 L2和 L3分别相交于两个第二辅助点 E和 D; 并获取两个第二辅助点 E和 D的坐标值 (x2 ,y2) 和 (xl,yl) 。 [0046] Step S1063, as shown in FIG. 4, select, among the two coordinate strips of the two light strips emitted by the first light source 1 adjacent to the opposite sides of the target point C as two first auxiliary points A and B, straight line AC and straight line BC near It seems to be a straight line LI; the auxiliary line passing through the origin 0 and the auxiliary point A is L2, the auxiliary line passing through the origin 0 and the auxiliary point B is L3, and the position of the second light source 2 is P(l, 0) and the auxiliary of the target point C The line L4 intersects the auxiliary lines L2 and L3 at the two second auxiliary points E and D, respectively; and acquires the coordinate values (x2, y2) and (xl, yl) of the two second auxiliary points E and D.
[0047] A点和 B点是第一光源 1发出的第 n条和第 n+1条亮条纹上的点, C点是第二光源 2 发出的第 m条亮条纹上的点, 根据光栅衍射原理和光栅常数、 光源波长等参数, n和 m是可以测量得知的已知自然数, 即, 辅助线 L2、 L3以及 L4分别与 x轴的夹 角 α、 β、 γ为可测量获知的, 即夹角 α、 β、 γ为已知, 而在图 4中, 第一光源 1和 第二光源 2的距离即线段 0Ρ也为已知。 则在三角形 ΕΟΡ中, 0Ρ的长度已知, 夹角 α和 γ已知, 则可计算得知 D点的坐标值 (xl,yl) , 同理, 可计算得知 E点的坐标 值 (x2,y2)。  [0047] Point A and Point B are points on the nth and n+1th bright stripes emitted by the first light source 1, and point C is a point on the mth bright stripe emitted by the second light source 2, according to the grating Parameters such as diffraction principle and grating constant, source wavelength, etc., n and m are known natural numbers that can be measured, that is, the angles α, β, and γ of the auxiliary lines L2, L3, and L4 with the x-axis are measurable. That is, the angles α, β, γ are known, and in Fig. 4, the distance between the first light source 1 and the second light source 2, that is, the line segment 0Ρ is also known. Then, in the triangle ΕΟΡ, the length of 0Ρ is known, and the angles α and γ are known, then the coordinate value (xl, yl) of the point D can be calculated. Similarly, the coordinate value of the point E can be calculated (x2 , y2).
[0048] 步骤 S1065 , 根据两个第二辅助点 E和 D的坐标值以及两个第一辅助点 A和 B与 C 的距离的比例关系, 获取目标点的坐标值。  [0048] Step S1065: Acquire coordinate values of the target point according to the coordinate values of the two second auxiliary points E and D and the proportional relationship between the distances of the two first auxiliary points A and B and C.
[0049] 线段 AC与 BC的长度比值可由相机 3拍摄的如图 2所示的亮条纹图像中测量得知 : C点为图 3中的某一已知亮条纹上的点, 测量与 C点相对两侧相邻的两条亮条纹 与 C点所在亮条纹的距离, 即计算亮条纹之间的在水平方向上的像素数, 可得到 线段 AC与 BC的长度比值。 本实施例中, 由于相邻条纹的间距相比于其与 X轴的 距离为很小, 所以可以将线段 EC与 DC的长度比值近似与线段 AC与 BC的长度比 值相等, 即, 因此可以根据点1)、 点 E的坐标以及 EC/DC的比值, 得到目标点 C 的坐标值。  [0049] The ratio of the length of the line segment AC to BC can be measured by the bright stripe image as shown in FIG. 2 taken by the camera 3: point C is a point on a known bright stripe in FIG. 3, measurement and point C The distance between the two bright stripes adjacent to the two sides and the bright stripes at the C point, that is, the number of pixels in the horizontal direction between the bright stripes is calculated, and the ratio of the lengths of the segments AC and BC can be obtained. In this embodiment, since the distance between adjacent stripes is smaller than the distance from the X axis, the ratio of the length of the line segment EC to DC can be approximately equal to the ratio of the lengths of the line segments AC and BC, that is, Point 1), the coordinates of point E, and the ratio of EC/DC, the coordinate value of the target point C is obtained.
[0050] 由上可知, 本申请上述步骤通过构建坐标系和辅助点, 实现了获取目标点的技 术目的。  [0050] As can be seen from the above, the above steps of the present application achieve the technical purpose of acquiring a target point by constructing a coordinate system and an auxiliary point.
[0051] 步骤 S1066, 将待测目标点 C替换为另一目标点, 重复步骤 S1061-S1065 , 直至 获取所有预定目标点的坐标值。  [0051] Step S1066: Replace the target point C to be replaced with another target point, and repeat steps S1061-S1065 until the coordinate values of all the predetermined target points are acquired.
[0052] 可选的, 根据本申请上述实施例, 在获取所述多个目标点的坐标值, 并根据所 述多个目标点的坐标值获取所述目标曲面之后, 方法还包括: [0052] Optionally, according to the foregoing embodiment of the present application, after acquiring the coordinate values of the plurality of target points, and acquiring the target surface according to the coordinate values of the plurality of target points, the method further includes:
[0053] 步骤 S110, 根据目标曲面确定目标曲面所属的飞艇副气囊的容积。 [0053] Step S110: Determine a volume of the airship sub-airbag to which the target curved surface belongs according to the target curved surface.
[0054] 具体的, 上述飞艇副气囊的容积用于表征副气囊的充气情况, 从而能够获取飞 艇的气囊的状态, 以及飞艇的飞行状态。 [0054] Specifically, the volume of the airship sub-airbag is used to characterize the inflation of the sub-bag, so that the fly can be obtained. The state of the airbag of the boat, and the flight status of the airship.
[0055] 步骤 S112, 获取预设的安全容积范围。  [0055] Step S112: Obtain a preset safety volume range.
[0056] 具体的, 上述预设的安全容积范围可以包括一个最大容积和一个最小容积。  [0056] Specifically, the preset safety volume range may include a maximum volume and a minimum volume.
[0057] 步骤 S114, 在飞艇副气囊的容积不处于安全容积范围的情况下, 发出报警信号 [0057] Step S114, when the volume of the airship sub-airbag is not in the safe volume range, an alarm signal is issued.
[0058] 具体的, 在飞艇副气囊的容积大于最大容积或小于最小容积的情况下, 确认飞 艇副气囊的容积不处于安全容积范围内, 因此副气囊处于非安全状态, 发出报 警信号。 还可以具有实吋数据显示装置, 用于实吋显示副气囊的容积。 [0058] Specifically, in a case where the volume of the airship sub-airbag is larger than the maximum volume or smaller than the minimum volume, it is confirmed that the volume of the airbag sub-airbag is not within the safe volume range, and therefore the sub-bag is in an unsafe state, and an alarm signal is issued. It is also possible to have a real data display device for displaying the volume of the sub-bag.
[0059] 需要说明的是, 飞艇副气囊内部填充空气, 处于飞艇主气囊内部, 且与之气囊 之间填充氦气, 通过主气囊与副气囊之间的氦气为飞艇提供浮力。 在一种可选 的实施例中, 由于副气囊的体积小于最小容积而产生报警信号, 则可以认为飞 艇主气囊体积过大, 可能是由于主气囊内气体温度过高而引起; 在另一种可选 的实施例中, 由于副气囊的体积大于最大容积而产生报警信号, 则可以认为飞 艇气囊体积过小, 可能是由于气囊气体温度过低而弓 I起。  [0059] It should be noted that the airbag sub-airbag is filled with air inside, is inside the airship main airbag, and is filled with helium gas, and the airship is provided with buoyancy through the helium between the main airbag and the sub-airbag. In an optional embodiment, if the volume of the sub-bag is less than the minimum volume and an alarm signal is generated, the airship main airbag may be considered to be too large, possibly due to excessive gas temperature in the main airbag; In an alternative embodiment, since the alarm signal is generated due to the volume of the sub-bag being larger than the maximum volume, the airbag airbag may be considered to be too small, possibly due to the air temperature of the airbag being too low.
[0060] 由上可知, 本申请上述步骤通过获取预设的安全容积范围, 在飞艇副气囊的容 积不处于安全容积范围的情况下, 发出报警信号, 实现了对飞艇副气囊的状态 的监控, 从而实现了对飞艇飞行状态的监控。  [0060] As can be seen from the above, the above steps of the present application obtain an initial safe volume range, and when the volume of the airship sub-airbag is not in the safe volume range, an alarm signal is issued, and the state of the airship sub-airbag is monitored. Thereby, the monitoring of the flight state of the airship is realized.
[0061] 可选的, 根据本申请上述实施例, 两台预设光源及用于采集图像的装置均设置 于飞艇副气囊内, 根据目标曲面确定目标曲面所属的飞艇副气囊的容积的方法 包括: 使用曲面上的目标点至光源的距离对曲面进行积分, 得到飞艇副气囊的 内部容积。  [0061] Optionally, according to the foregoing embodiment of the present application, two preset light sources and devices for acquiring images are disposed in the airbag sub-airbag, and the method for determining the volume of the airship sub-airbag to which the target curved surface belongs according to the target curved surface includes: : Integrate the surface using the distance from the target point on the surface to the source to obtain the internal volume of the airship sub-balloon.
[0062] 在一种可选的实施例中, 以图 2所示的示例进行描述, 203为飞艇副气囊的目标 曲面, 也即相机拍摄到的部分, 第一光源 1和第二光源 2都处于飞艇副气囊内部 , 在获取到目标曲面之后, 实际可以得到以第一光源 1为锥顶, 以曲面 203为底 面的椎体, 由于获取到了目标曲面上每个目标点的坐标, 因此能够知晓曲面 203 上每个目标点距离锥顶光源 1的距离, 使用曲面 203上的目标点至光源 1的距离对 曲面 203进行积分, 能够得到椎体的体积, 通过椎体的体积则能够得到飞艇副气 囊的内部容积。 [0063] 实施例 2 [0062] In an alternative embodiment, described with the example shown in FIG. 2, 203 is the target curved surface of the airship sub-balloon, that is, the portion photographed by the camera, the first light source 1 and the second light source 2 are both In the airbag sub-airbag, after the target curved surface is acquired, the vertebral body with the first light source 1 as the cone top and the curved surface 203 as the bottom surface can be obtained, and since the coordinates of each target point on the target curved surface are acquired, it can be known. The distance from each target point on the curved surface 203 to the cone-top light source 1 is integrated with the distance from the target point on the curved surface 203 to the light source 1 to obtain the volume of the vertebral body. The volume of the vertebral body can be obtained by the volume of the vertebral body. The internal volume of the airbag. Example 2
[0064] 根据实施例 1提供的获取目标曲面的方法, 本申请还提供了一种获取目标曲面 的装置, 图 5是根据本发明实施例的一种获取目标曲面的装置的结构示意图, 该 装置包括:  [0064] According to the method for acquiring a target curved surface provided by Embodiment 1, the present application further provides an apparatus for acquiring a target curved surface, and FIG. 5 is a schematic structural diagram of an apparatus for acquiring a target curved surface according to an embodiment of the present invention. Includes:
[0065] 采集模块 50, 用于采集由光线投射在目标曲面上而产生的图像, 图像包括: 多 个亮条纹, 其中, 光线为两台预设光源发出的出射光线, 分别来自两台预设光 源的亮条纹间隔排列。  [0065] The acquisition module 50 is configured to collect an image generated by the light being projected on the target curved surface, where the image includes: a plurality of bright stripes, wherein the light is the outgoing light emitted by the two preset light sources, respectively, from the two presets. The light strips of the light source are arranged at intervals.
[0066] 具体的, 上述目标曲面为需要监测的副气囊的表面, 在上述步骤中, 可以由相 机来采集含有多个亮条纹的图像。  [0066] Specifically, the target curved surface is a surface of a sub-balloon to be monitored, and in the above step, an image containing a plurality of bright stripes may be collected by a camera.
[0067] 在一种可选的实施例中, 上述亮条纹可以是对预设光源的出射光线进行分束调 制得到, 由于预设光源的出射光线经过分束调制会得到间隔排列的亮暗线, 间 隔排列的亮暗线会在副气囊避免构成多个亮条纹, 再采用相机采集多个亮条纹 构成的图像。 [0067] In an optional embodiment, the bright stripe may be obtained by splitting and modulating the outgoing light of the preset light source, and the light emitted by the preset light source is split and modulated to obtain bright and dark lines arranged at intervals. The bright and dark lines arranged at intervals will avoid the formation of multiple bright stripes in the sub-balloon, and then the camera will capture images of multiple bright stripes.
[0068] 具体的, 上述目标点用于确定目标曲面。  [0068] Specifically, the target point is used to determine a target curved surface.
[0069] 此处需要说明的是, 亮条纹的间距不同, 取目标点的密集程度也不一定相同, 因此同一个目标曲面的监测精度也会受到多个亮条纹的间距以及取目标点的密 集程度的影响, 在取得的目标点较多的情况下, 监测得到的目标曲面更精确, 但由于目标点较多, 计算量也较大, 在取得的目标点较少的情况下, 监测得到 的目标曲面不够精确, 但数据计算量较小, 因此可以根据实际的监测要求来取 得目标点。  [0069] It should be noted that the spacing of the bright stripes is different, and the density of the target points is not necessarily the same. Therefore, the monitoring accuracy of the same target surface is also affected by the spacing of multiple bright stripes and the concentration of the target points. The degree of influence, in the case of more target points obtained, the target surface obtained by the monitoring is more accurate, but the calculation amount is larger due to more target points, and the monitoring result is obtained when the target points are small. The target surface is not precise enough, but the amount of data calculation is small, so the target point can be obtained according to the actual monitoring requirements.
[0070] 第一获取模块 52, 用于从所述图像中的亮条纹上取多个目标点。  [0070] The first obtaining module 52 is configured to take a plurality of target points from the bright stripes in the image.
[0071] 第二获取模块 54, 用于获取多个目标点的坐标值, 并根据多个目标点的坐标值 获取目标曲面。  [0071] The second obtaining module 54 is configured to acquire coordinate values of the plurality of target points, and acquire the target curved surface according to the coordinate values of the plurality of target points.
[0072] 在上述装置中, 由于光源为预设的光源, 因此光源与目标曲面的距离是已知的 , 在确定目标点之后, 可以根据光源与目标曲面之间的距离关系, 计算每个目 标点的坐标值, 在一种可选的实施例中, 可以根据三维立体重构方法直接得到 相似度较高的目标曲面。 本实施例中的三维立体重构方法可以为如实施例 1中的 步骤 S1061-S1066所述的方法。 [0073] 确定模块, 用于根据目标曲面确定副气囊的容积。 [0072] In the above device, since the light source is a preset light source, the distance between the light source and the target curved surface is known, and after determining the target point, each target can be calculated according to the distance relationship between the light source and the target curved surface. The coordinate value of the point, in an optional embodiment, the target surface with higher similarity can be directly obtained according to the three-dimensional reconstruction method. The three-dimensional stereo reconstruction method in this embodiment may be the method as described in steps S1061-S1066 in Embodiment 1. [0073] a determining module, configured to determine a volume of the sub-airbag according to the target curved surface.
[0074] 此处需要说明的是, 上述实施例提供的获取目标曲面的方法所适用的环境适应 性较好、 系统搭建简单、 图像处理明了、 成本低廉。 除了应用于飞艇副气囊监 控之外, 还可以应用于制作双补光灯立体成像相机、 暗室环境下的三维重构应 用等。 能够在这些场景中发挥三维重构、 立体拍照、 目标位置监测、 立体成像 重构的作用。  [0074] It should be noted that the method for obtaining a target curved surface provided by the above embodiment is applicable to the environment adaptability, the system is simple to construct, the image processing is clear, and the cost is low. In addition to being used for airship sub-airbag monitoring, it can also be used to make dual-filler stereo imaging cameras and 3D reconstruction applications in darkroom environments. It can play the role of 3D reconstruction, stereo photography, target position monitoring, and stereo imaging reconstruction in these scenes.
[0075] 由上可知, 本申请上述装置通过采集模块采集由光线投射在目标曲面上而产生 的图像, 通过第一获取模块从图像中的亮条纹上取多个目标点, 通过第二获取 模块获取多个目标点的坐标值, 并根据多个目标点的坐标值获取目标曲面, 并 通过确定模块根据目标曲面确定副气囊的容积。 上述方案环境适用性强, 使用 过程中即使光源和相机的姿态发生较大的变化, 也无需校准, 并可以有效的监 测出副气囊的状况, 监测的精度也能满足实际需求。  [0075] It can be seen from the above that the foregoing device of the present application collects an image generated by the light being projected on the target curved surface by the acquiring module, and adopts the first acquiring module to take a plurality of target points from the bright stripes in the image, and adopts the second acquiring module. Obtain coordinate values of multiple target points, and obtain a target surface according to coordinate values of the plurality of target points, and determine a volume of the sub-airbag according to the target curved surface by the determining module. The above scheme has strong applicability, and even if the attitude of the light source and the camera changes greatly during use, calibration is not required, and the condition of the sub-balloon can be effectively monitored, and the accuracy of the monitoring can also meet the actual demand.
[0076] 可选的, 根据本申请上述实施例, 上述装置还包括: 生成模块, 用于在采集由 光线投射在目标曲面上而产生的图像之前, 生成亮条纹, 其中, 生成模块包括  [0076] Optionally, according to the foregoing embodiment of the present application, the foregoing apparatus further includes: a generating module, configured to generate a bright stripe before acquiring an image generated by the ray being projected on the target curved surface, where the generating module includes
[0077] 设置单元, 用于在目标曲面前方设置间隔预设距离的两台预设光源。 [0077] a setting unit, configured to set two preset light sources spaced apart by a preset distance in front of the target curved surface.
[0078] 调制单元, 用于对两台预设光源的出射光线进行分束调制, 使出射光线形成亮 条纹。  [0078] a modulating unit, configured to perform beam splitting modulation on the outgoing light of the two preset light sources, so that the outgoing light forms a bright stripe.
[0079] 由上可知, 本申请上述装置通过设置单元在目标曲面前方设置间隔预设距离的 两台预设光源, 通过调制单元对两台预设光源的出射光线进行分束调制, 使出 射光线形成亮条纹。 上述方案通过在目标曲面前方设置光源, 并对光源进行分 束调制, 形成了用于获取目标点的图像。  [0079] As can be seen from the above, the above-mentioned device of the present application sets two preset light sources spaced apart by a preset distance in front of the target curved surface by the setting unit, and splits and modulates the emitted light of the two preset light sources through the modulating unit to make the outgoing light. Form bright stripes. The above scheme forms an image for acquiring a target point by setting a light source in front of the target curved surface and splitting the light source.
[0080] 可选的, 根据本申请上述实施例, 第一获取模块 52包括: [0080] Optionally, according to the foregoing embodiment of the present application, the first obtaining module 52 includes:
[0081] 第一获取单元, 用于对采集的图像取等间距直线, 其中, 直线与亮条纹相交。 [0081] The first acquiring unit is configured to take an equally spaced line of the captured image, where the straight line intersects the bright stripe.
[0082] 第一确定单元, 用于确定直线与亮条纹的交点为多个目标点。 [0082] The first determining unit is configured to determine that an intersection of the straight line and the bright stripe is a plurality of target points.
[0083] 可选的, 根据本申请上述实施例, 第二获取模块 54包括: [0083] Optionally, according to the foregoing embodiment of the present application, the second obtaining module 54 includes:
[0084] 第二确定单元, 用于确定所述两台预设光源中第一光源 1为原点, 所述第一光 源 1与第二光源 2的连线作为第一维度, 确定在预设平面上与所述第一维度垂直 的方向为第二维度, 其中, 所述预设平面为由所述两台预设光源与一待测的目 标点确定的平面, 所述待测的目标点对应于所述第二光源 2发出的一亮条纹, 所 述待测的目标点对应于所述第二光源 2发出的一亮条纹。 [0084] The second determining unit is configured to determine that the first light source 1 of the two preset light sources is an origin, and the connection between the first light source 1 and the second light source 2 is used as a first dimension, and is determined in a preset plane. Vertically perpendicular to the first dimension The direction is a second dimension, where the preset plane is a plane determined by the two preset light sources and a target point to be tested, and the target point to be tested corresponds to the second light source 2 a bright stripe, the target point to be measured corresponds to a bright stripe emitted by the second light source 2.
[0085] 建立单元, 用于根据第一维度和第二维度建立坐标系; [0085] an establishing unit, configured to establish a coordinate system according to the first dimension and the second dimension;
[0086] 第二获取单元, 用于在坐标系中选取与目标点两侧相邻的由第一光源 1发出的 两条亮条纹中的亮点作为两个第一辅助点, 第二光源 2与所述目标点的连线与两 条辅助线的交点为两个第二辅助点, 其中, 两条辅助线为第一光源 1与所述第一 辅助点的连线;  [0086] a second acquiring unit, configured to select, in the coordinate system, a bright point among two bright stripes emitted by the first light source 1 adjacent to the two sides of the target point as the two first auxiliary points, and the second light source 2 and The intersection of the line connecting the target point and the two auxiliary lines is two second auxiliary points, wherein the two auxiliary lines are the connection between the first light source 1 and the first auxiliary point;
[0087] 第三获取单元, 用于根据第二辅助点的坐标值以及第一辅助点的距离的比例, 获取目标点的坐标值。  [0087] The third obtaining unit is configured to acquire a coordinate value of the target point according to a coordinate value of the second auxiliary point and a ratio of the distance of the first auxiliary point.
[0088] 可选的, 根据本申请上述实施例, 上述装置还包括: [0088] Optionally, according to the foregoing embodiment of the present application, the foregoing apparatus further includes:
[0089] 确定模块, 用于根据目标曲面确定目标曲面所属的飞艇副气囊的容积; [0089] a determining module, configured to determine, according to the target curved surface, a volume of the airship sub-airbag to which the target curved surface belongs;
[0090] 第三获取模块, 用于获取预设的安全容积范围; [0090] a third obtaining module, configured to acquire a preset safety volume range;
[0091] 报警模块, 用于在飞艇副气囊的容积不处于安全容积范围的情况下, 发出报警 信号。  [0091] The alarm module is configured to issue an alarm signal when the volume of the airship sub-airbag is not within a safe volume range.
[0092] 实施例 3 Example 3
[0093] 根据实施例 1提供的获取目标曲面的方法, 本申请还提供了一种获取目标曲面 的系统, 图 6是根据本发明实施例的一种获取目标曲面的系统的结构示意图, 该 装置包括:  [0093] According to the method for acquiring a target curved surface provided by Embodiment 1, the present application further provides a system for acquiring a target curved surface, and FIG. 6 is a schematic structural diagram of a system for acquiring a target curved surface according to an embodiment of the present invention. Includes:
[0094] 两台预设光源 60, 用于发出的出射光线。  [0094] Two preset light sources 60 for emitting outgoing light.
[0095] 具体的, 上述目标曲面为需要监测的副气囊的表面, 在上述步骤中, 可以由相 机来采集含有多个亮条纹的图像。  [0095] Specifically, the target curved surface is a surface of a sub-balloon to be monitored, and in the above step, an image containing a plurality of bright stripes may be collected by a camera.
[0096] 在一种可选的实施例中, 上述多个亮条纹可以是对光源的出射光线进行分束调 制得到, 由于光源的出射光线经过分束调制会得到间隔排列的亮暗线, 间隔排 列的亮暗线会在副气囊避免构成多个亮条纹, 再采用相机采集亮条纹构成的图 像。 [0096] In an optional embodiment, the plurality of bright stripes may be obtained by splitting and modulating the outgoing light of the light source, and the light emitted by the light source is split and modulated to obtain bright and dark lines arranged at intervals. The bright and dark lines will avoid multiple bright stripes in the sub-balloon, and then use the camera to capture the image of the bright stripes.
[0097] 图像采集设备 62, 用于采集由出射光线投射在目标曲面上而产生的图像, 图像 包括: 亮条纹, 目标曲面为副气囊的表面。 [0098] 具体的, 上述目标点用于确定目标曲面。 [0097] The image capturing device 62 is configured to collect an image generated by the projected light being projected on the target curved surface, and the image includes: a bright stripe, and the target curved surface is a surface of the sub-balloon. [0098] Specifically, the target point is used to determine a target curved surface.
[0099] 此处需要说明的是, 亮条纹的间距不同, 取目标点的密集程度也不一定相同, 因此同一个目标曲面的监测精度也会受到亮条纹的间距以及取目标点的密集程 度的影响, 在取得的目标点较多的情况下, 监测得到的目标曲面更精确, 但由 于目标点较多, 计算量也较大, 在取得的目标点较少的情况下, 监测得到的目 标曲面不够精确, 但数据计算量较小, 因此可以根据实际的监测要求来取得目 标点。  [0099] It should be noted here that the spacing of the bright stripes is different, and the density of the target points is not necessarily the same, so the monitoring accuracy of the same target surface is also affected by the spacing of the bright stripes and the density of the target points. Influence, in the case where there are many target points obtained, the target surface obtained by the monitoring is more accurate, but the calculation amount is larger due to more target points, and the target surface is monitored when the target points are small. Not precise enough, but the amount of data calculation is small, so you can get the target point according to the actual monitoring requirements.
[0100] 处理器 64, 与图像采集设备相连, 用于从图像中的亮条纹上取多个目标点; 获 取多个目标点的坐标值, 根据多个目标点的坐标值获取目标曲面; 并根据目标 曲面确定副气囊的容积。  [0100] The processor 64 is connected to the image capturing device, and is configured to take a plurality of target points from the bright stripes in the image; acquire coordinate values of the plurality of target points, and obtain a target surface according to the coordinate values of the plurality of target points; The volume of the sub-bag is determined according to the target surface.
[0101] 在上述系统中, 由于光源为预设的光源, 因此光源与目标曲面的距离是已知的 [0101] In the above system, since the light source is a preset light source, the distance between the light source and the target curved surface is known.
, 在确定目标点之后, 可以根据光源与目标曲面之间的距离关系, 计算每个目 标点的坐标值, 在一种可选的实施例中, 可以根据三维立体重构方法直接得到 相似度较高的目标曲面。 After determining the target point, the coordinate value of each target point can be calculated according to the distance relationship between the light source and the target surface. In an optional embodiment, the similarity can be directly obtained according to the three-dimensional reconstruction method. High target surface.
[0102] 此处需要说明的是, 上述实施例提供的获取目标曲面的方法所适用的环境适应 性较好、 系统搭建简单、 图像处理明了、 成本低廉。 除了应用于飞艇副气囊监 控之外, 还可以应用于制作双补光灯立体成像相机、 暗室环境下的三维重构应 用等。 能够在这些场景中发挥三维重构、 立体拍照、 目标位置监测、 立体成像 重构的作用。  [0102] It should be noted that the method for obtaining a target curved surface provided by the above embodiment is applicable to the environment adaptability, the system is simple to construct, the image processing is clear, and the cost is low. In addition to being used for airship sub-airbag monitoring, it can also be used to make dual-filler stereo imaging cameras and 3D reconstruction applications in darkroom environments. It can play the role of 3D reconstruction, stereo photography, target position monitoring, and stereo imaging reconstruction in these scenes.
[0103] 由上可知, 本申请上述系统通过预设光源发出的出射光线, 通过图像采集设备 采集由出射光线投射在目标曲面上而产生的图像, 通过处理器与图像采集设备 相连, 从图像中的亮条纹上取多个目标点; 获取多个目标点的坐标值, 根据多 个目标点的坐标值获取目标曲面; 并根据目标曲面确定副气囊的容积。 上述方 案环境适用性强, 使用过程中即使光源和相机的姿态发生较大的变化, 也无需 校准, 并可以有效的监测出副气囊的状况, 监测的精度也能满足实际需求。  [0103] It can be seen from the above that the above-mentioned system of the present application collects an image generated by the emitted light on the target curved surface through an image capturing device by using the emitted light emitted by the preset light source, and is connected to the image collecting device through the processor, from the image. The plurality of target points are taken on the bright stripe; the coordinate values of the plurality of target points are obtained, the target surface is obtained according to the coordinate values of the plurality of target points; and the volume of the sub-bag is determined according to the target surface. The above-mentioned scheme has strong applicability. Even if the attitude of the light source and the camera changes greatly during use, there is no need to calibrate, and the condition of the sub-balloon can be effectively monitored, and the accuracy of the monitoring can also meet the actual demand.
[0104] 可选的, 根据本申请上述实施例, 上述系统还包括: 预设光源为两台光源, 设 置于目标曲面前方, 并与目标曲面间隔预设距离。  Optionally, according to the foregoing embodiment of the present application, the system further includes: the preset light source is two light sources disposed in front of the target curved surface and spaced apart from the target curved surface by a predetermined distance.
[0105] 图 2是根据本发明实施例的一种可选的光源和相机的分布示意图, 在一种可选 的情况下, 结合图 2所示的示例, 光源为近红外光源, 放置于目标曲面前, 以两 个光源的出射光在目标曲面上具有一定的重复覆盖面, 用于采集图像的相机位 于两个近红外光源之间, 用于采集近红外光源的出射光线构成的多个亮条纹。 2 is a schematic diagram of an alternative light source and camera distribution, in an optional manner, in accordance with an embodiment of the present invention. In the case of the example shown in FIG. 2, the light source is a near-infrared light source placed in front of the target curved surface, and the emitted light of the two light sources has a certain repeated coverage on the target curved surface, and the camera for acquiring images is located at two. Between the near-infrared light sources, a plurality of bright stripes formed by the emitted light of the near-infrared light source.
[0106] 此处需要说明的是, 上述相机以及光源的分布位置并不一定局限于上述实施例 , 在知晓两个光源之间的距离, 以及两个光源分别与目标曲面的处置距离的情 况下, 就能够获取到目标点的坐标值。  [0106] It should be noted here that the distribution position of the camera and the light source is not necessarily limited to the above embodiment, and the distance between the two light sources and the disposal distance between the two light sources and the target curved surface are known. , you can get the coordinates of the target point.
[0107] 上述本发明实施例序号仅仅为了描述, 不代表实施例的优劣。  [0107] The foregoing serial numbers of the embodiments of the present invention are merely for the description, and do not represent the advantages and disadvantages of the embodiments.
[0108] 在本发明的上述实施例中, 对各个实施例的描述都各有侧重, 某个实施例中没 有详述的部分, 可以参见其他实施例的相关描述。  [0108] In the above-described embodiments of the present invention, the descriptions of the various embodiments are different, and the detailed description of the other embodiments may be referred to.
[0109] 在本申请所提供的几个实施例中, 应该理解到, 所揭露的技术内容, 可通过其 它的方式实现。 其中, 以上所描述的装置实施例仅仅是示意性的, 例如所述单 元的划分, 可以为一种逻辑功能划分, 实际实现吋可以有另外的划分方式, 例 如多个单元或组件可以结合或者可以集成到另一个系统, 或一些特征可以忽略 , 或不执行。 另一点, 所显示或讨论的相互之间的耦合或直接耦合或通信连接 可以是通过一些接口, 单元或模块的间接耦合或通信连接, 可以是电性或其它 的形式。  [0109] In the several embodiments provided by the present application, it should be understood that the disclosed technical content may be implemented in other manners. The device embodiments described above are only schematic. For example, the division of the unit may be a logical function division. The actual implementation may have another division manner. For example, multiple units or components may be combined or may be Integration into another system, or some features can be ignored, or not executed. In addition, the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, unit or module, and may be electrical or otherwise.
[0110] 所述作为分离部件说明的单元可以是或者也可以不是物理上分幵的, 作为单元 显示的部件可以是或者也可以不是物理单元, 即可以位于一个地方, 或者也可 以分布到多个单元上。 可以根据实际的需要选择其中的部分或者全部单元来实 现本实施例方案的目的。  [0110] The unit described as a separate component may or may not be physically distributed, and the component displayed as a unit may or may not be a physical unit, that is, may be located in one place, or may be distributed to multiple On the unit. Some or all of the units may be selected according to actual needs to achieve the objectives of the embodiment of the present embodiment.
[0111] 另外, 在本发明各个实施例中的各功能单元可以集成在一个处理单元中, 也可 以是各个单元单独物理存在, 也可以两台或两台以上单元集成在一个单元中。 上述集成的单元既可以采用硬件的形式实现, 也可以采用软件功能单元的形式 实现。  In addition, each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit. The above integrated unit can be implemented in the form of hardware or in the form of a software functional unit.
[0112] 所述集成的单元如果以软件功能单元的形式实现并作为独立的产品销售或使用 吋, 可以存储在一个计算机可读取存储介质中。 基于这样的理解, 本发明的技 术方案本质上或者说对现有技术做出贡献的部分或者该技术方案的全部或部分 可以以软件产品的形式体现出来, 该计算机软件产品存储在一个存储介质中, 包括若干指令用以使得一台计算机设备 (可为个人计算机、 服务器或者网络设 备等) 执行本发明各个实施例所述方法的全部或部分步骤。 而前述的存储介质 包括: U盘、 只读存储器 (ROM, Read-Only [0112] The integrated unit, if implemented in the form of a software functional unit and sold or used as a standalone product, may be stored in a computer readable storage medium. Based on such understanding, the technical solution of the present invention may contribute to the prior art or all or part of the technical solution may be embodied in the form of a software product stored in a storage medium. , A number of instructions are included to cause a computer device (which may be a personal computer, server or network device, etc.) to perform all or part of the steps of the methods described in various embodiments of the present invention. The foregoing storage medium includes: a USB flash drive, a read only memory (ROM, Read-Only)
Memory) 、 随机存取存储器 (RAM, Random Access Memory) 、 移动硬盘、 磁 碟或者光盘等各种可以存储程序代码的介质。  Memory, Random Access Memory (RAM), removable hard disk, disk or optical disk, and other media that can store program code.
以上所述仅是本发明的优选实施方式, 应当指出, 对于本技术领域的普通技术 人员来说, 在不脱离本发明原理的前提下, 还可以做出若干改进和润饰, 这些 改进和润饰也应视为本发明的保护范围。  The above description is only a preferred embodiment of the present invention, and it should be noted that those skilled in the art can also make several improvements and retouchings without departing from the principles of the present invention. It should be considered as the scope of protection of the present invention.

Claims

权利要求书 Claim
[权利要求 1] 一种获取目标曲面的方法, 其特征在于, 包括:  [Claim 1] A method for acquiring a target curved surface, comprising:
采集由光线投射在目标曲面上而产生的图像, 所述图像包括: 多个亮 条纹, 其中, 所述光线为两台预设光源发出的出射光线, 分别来自所 述两台预设光源的亮条纹间隔排列;  Collecting an image generated by the light being projected on the target surface, the image comprising: a plurality of bright stripes, wherein the light is an outgoing light emitted by two preset light sources, respectively, from the brightness of the two preset light sources Stripe spacing;
从所述图像中的亮条纹上取多个目标点;  Taking a plurality of target points from the bright stripes in the image;
获取所述多个目标点的坐标值, 并根据所述多个目标点的坐标值获取 所述目标曲面。  Obtaining coordinate values of the plurality of target points, and acquiring the target curved surface according to coordinate values of the plurality of target points.
[权利要求 2] 根据权利要求 1所述的方法, 其特征在于, 在采集由光线投射在目标 曲面上而产生的图像之前, 所述方法还包括: 生成所述亮条纹, 其中 , 生成所述亮条纹的步骤包括:  [Claim 2] The method according to claim 1, wherein before the image generated by the ray is projected on the target curved surface, the method further comprises: generating the bright stripe, wherein The steps of bright stripes include:
在所述目标曲面前方设置间隔预设距离的两台所述预设光源; 对两台所述预设光源的出射光线进行分束调制, 使所述出射光线形成 所述多个亮条纹。  Two preset light sources spaced apart by a predetermined distance are disposed in front of the target curved surface; and the emitted light of the two preset light sources is split-modulated, so that the emergent light forms the plurality of bright stripes.
[权利要求 3] 根据权利要求 2所述的方法, 其特征在于, 从所述图像中的亮条纹上 取多个目标点, 包括:  [Claim 3] The method according to claim 2, wherein: taking a plurality of target points from the bright stripes in the image comprises:
对采集的所述图像取等间距直线, 其中, 所述直线与所述多个亮条纹 相交;  Taking the acquired image as an equidistant straight line, wherein the straight line intersects the plurality of bright stripes;
确定所述直线与所述亮条纹的交点为所述多个目标点。  Determining an intersection of the straight line and the bright stripe as the plurality of target points.
[权利要求 4] 根据权利要求 3所述的方法, 其特征在于, 获取所述多个目标点的坐 标值, 包括: [Claim 4] The method according to claim 3, wherein obtaining the coordinate values of the plurality of target points comprises:
所述两台预设光源为第一光源和第二光源, 确定所述两台预设光源中 第一光源为原点, 所述第一光源与第二光源的连线为第一维度, 确定 在预设平面上与所述第一维度垂直的方向为第二维度, 其中, 所述预 设平面为由所述两台预设光源与一待测的目标点确定的平面, 所述待 测的目标点对应于所述第二光源发出的一亮条纹; 根据所述第一维度和所述第二维度建立坐标系; 在坐标系中选取与所述目标点两侧相邻的由所述第一光源发出的两条 亮条纹中的亮点作为两个第一辅助点, 所述第二光源与所述目标点的 连线与两条辅助线的交点为两个第二辅助点, 其中, 所述两条辅助线 为所述第一光源与所述两个第一辅助点的连线; 根据所述两个第二辅助点的坐标值以及所述两个第一辅助点与所述待 测的目标点的距离的比例关系, 获取所述目标点的坐标值。 The two preset light sources are a first light source and a second light source, and the first light source of the two preset light sources is determined as an origin, and the connection between the first light source and the second light source is a first dimension, and The direction perpendicular to the first dimension on the preset plane is a second dimension, where the preset plane is a plane determined by the two preset light sources and a target point to be tested, and the to-be-tested The target point corresponds to a bright stripe emitted by the second light source; a coordinate system is established according to the first dimension and the second dimension; and the second side adjacent to the target point is selected in the coordinate system by the first Two light sources The bright spot in the bright stripe is the two first auxiliary points, and the intersection of the line connecting the second source and the target point and the two auxiliary lines is two second auxiliary points, wherein the two auxiliary lines are a line connecting the first light source and the two first auxiliary points; according to coordinate values of the two second auxiliary points and a distance between the two first auxiliary points and the target point to be tested The proportional relationship obtains the coordinate value of the target point.
[权利要求 5] 根据权利要求 4所述的方法, 其特征在于, 根据所述两个第二辅助点 的坐标值以及所述两个第一辅助点与所述待测的目标点的距离的比例 关系, 获取所述目标点的坐标值, 包括: [Claim 5] The method according to claim 4, wherein: according to the coordinate values of the two second auxiliary points and the distance between the two first auxiliary points and the target point to be tested a proportional relationship, obtaining coordinate values of the target point, including:
根据对所述图像进行测量得到所述两个第一辅助点至所述待测的目标 点的距离的比例值;  And obtaining a ratio value of the distance between the two first auxiliary points to the target point to be tested according to the measurement of the image;
将所述两个第一辅助点至所述待测的目标点的距离的比例值作为所述 两个第二辅助点至所述待测的目标点的距离的比例值;  And a ratio value of a distance between the two first auxiliary points to the target point to be tested is a ratio of distances between the two second auxiliary points to the target point to be tested;
根据所述两个第二辅助点的坐标值和所述两个第二辅助点至所述目标 点的距离的比例值, 得到所述待测的目标点的坐标值。  And obtaining coordinate values of the target point to be tested according to a coordinate value of the coordinate values of the two second auxiliary points and a distance between the two second auxiliary points and the target point.
[权利要求 6] 根据权利要求 1至 5中任意一项所述的方法, 其特征在于, 所述目标曲 面为一飞艇的副气囊的表面。  [Claim 6] The method according to any one of claims 1 to 5, wherein the target curved surface is a surface of a sub-airbag of an airship.
[权利要求 7] 根据权利要求 6所述的方法, 其特征在于, 在获取所述多个目标点的 坐标值, 并根据所述多个目标点的坐标值获取所述目标曲面之后, 所 述方法还包括:  [Claim 7] The method according to claim 6, wherein after acquiring the coordinate values of the plurality of target points and acquiring the target curved surface according to the coordinate values of the plurality of target points, the The method also includes:
根据所述目标曲面确定所述目标曲面所属的飞艇副气囊的容积; 获取预设的安全容积范围;  Determining, according to the target curved surface, a volume of the airship sub-airbag to which the target curved surface belongs; acquiring a preset safe volume range;
在所述飞艇副气囊的容积不处于所述安全容积范围的情况下, 发出报 警信号。  An alarm signal is issued if the volume of the airship sub-airbag is not within the safe volume range.
[权利要求 8] 根据权利要求 7所述的方法, 其特征在于, 所述两台预设光源及用于 采集图像的装置均设置于所述飞艇副气囊内, 根据所述目标曲面确定 所述目标曲面所属的飞艇副气囊的容积的方法包括: 使用所述曲面上 的目标点至光源的距离对所述曲面进行积分, 得到飞艇副气囊的内部 容积。 一种获取目标曲面的装置, 其特征在于, 包括: [Claim 8] The method according to claim 7, wherein the two preset light sources and the means for acquiring images are disposed in the airship sub-airbag, and the determining is performed according to the target curved surface. The method for the volume of the airship sub-airbag to which the target surface belongs includes: integrating the curved surface using a distance from the target point to the light source on the curved surface to obtain an internal volume of the airship sub-airbag. A device for acquiring a target curved surface, comprising:
采集模块, 用于采集由光线投射在目标曲面上而产生的图像, 所述图 像包括: 多个亮条纹, 其中, 所述光线为两台预设光源发出的出射光 线, 分别来自所述两台预设光源的亮条纹间隔排列; An acquisition module, configured to collect an image generated by the light being projected on the target surface, the image comprising: a plurality of bright stripes, wherein the light is an outgoing light emitted by two preset light sources, respectively, from the two The light strips of the preset light source are arranged at intervals;
第一获取模块, 用于从所述图像中的亮条纹上取多个目标点; 第二获取模块, 用于获取所述多个目标点的坐标值, 并根据所述多个 目标点的坐标值获取所述目标曲面。 a first acquiring module, configured to take a plurality of target points from the bright stripe in the image; a second acquiring module, configured to acquire coordinate values of the plurality of target points, and according to coordinates of the multiple target points The value gets the target surface.
根据权利要求 9所述的装置, 其特征在于, 所述装置还包括: 生成模 块, 用于在采集由光线投射在目标曲面上而产生的图像之前, 生成所 述亮条纹, 其中, 所述生成模块包括: The device according to claim 9, wherein the device further comprises: a generating module, configured to generate the bright stripe before acquiring an image generated by the ray being projected on the target curved surface, wherein the generating Modules include:
设置单元, 用于在所述目标曲面前方设置间隔预设距离的两台所述预 设光源; a setting unit, configured to set two preset light sources spaced apart by a preset distance in front of the target curved surface;
调制单元, 用于对两台所述预设光源的出射光线进行分束调制, 使所 述出射光线形成所述亮条纹。 And a modulating unit, configured to perform beam splitting modulation on the outgoing rays of the two preset light sources, so that the emergent light forms the bright stripes.
根据权利要求 10所述的装置, 其特征在于, 所述第一获取模块包括: 第一获取单元, 用于对采集的所述图像取等间距直线, 其中, 所述直 线与所述多个亮条纹相交; The device according to claim 10, wherein the first obtaining module comprises: a first acquiring unit, configured to take an equidistant straight line to the collected image, wherein the straight line and the plurality of bright lines Stripes intersect;
第一确定单元, 用于确定所述直线与所述亮条纹的交点为所述多个目 标点。 And a first determining unit, configured to determine that an intersection of the straight line and the bright stripe is the plurality of target points.
根据权利要求 11所述的装置, 其特征在于, 所述两台预设光源为第一 光源和第二光源, 所述第二获取模块包括: The device according to claim 11, wherein the two preset light sources are a first light source and a second light source, and the second acquiring module comprises:
第二确定单元, 用于确定所述两台预设光源中第一光源为原点, 所述 第一光源与第二光源的连线作为第一维度, 确定在预设平面上与所述 第一维度垂直的方向为第二维度, 其中, 所述预设平面为由所述两台 预设光源与一待测的目标点确定的平面, 所述待测的目标点对应于所 述第二光源发出的一亮条纹, 所述待测的目标点对应于所述第二光源 发出的一亮条纹; a second determining unit, configured to determine that the first light source of the two preset light sources is an origin, and the connection between the first light source and the second light source is used as a first dimension, and is determined to be on the preset plane and the first The direction perpendicular to the dimension is a second dimension, where the preset plane is a plane determined by the two preset light sources and a target point to be tested, and the target point to be tested corresponds to the second light source a bright stripe emitted, the target point to be tested corresponds to a bright stripe emitted by the second light source;
建立单元, 用于根据所述第一维度和所述第二维度建立坐标系; 第二获取单元, 用于在坐标系中选取与所述待测的目标点两侧相邻的 由所述第一光源发出的两条亮条纹中的亮点作为两个第一辅助点, 所 述第二光源与所述目标点的连线与两条辅助线的交点为两个第二辅助 点, 其中, 所述两条辅助线为所述第一光源与所述第一辅助点的连线 第三获取单元, 用于根据所述第二辅助点的坐标值以及所述第一辅助 点与所述待测的目标点的距离的比例, 获取所述目标点的坐标值。 a establishing unit, configured to establish a coordinate system according to the first dimension and the second dimension; a second acquiring unit, configured to select, in the coordinate system, a bright spot among the two bright stripes emitted by the first light source adjacent to the two sides of the target point to be tested as the two first auxiliary points, where The intersection of the line connecting the second light source and the target point and the two auxiliary lines is two second auxiliary points, wherein the two auxiliary lines are the connection between the first light source and the first auxiliary point a third acquiring unit, configured to acquire a coordinate value of the target point according to a coordinate value of the second auxiliary point and a ratio of a distance between the first auxiliary point and the target point to be tested.
[权利要求 13] 根据权利要求 9至 12中任意一项所述的装置, 其特征在于, 所述装置 还包括: [Claim 13] The device according to any one of claims 9 to 12, wherein the device further comprises:
确定模块, 用于根据所述目标曲面确定所述目标曲面所属的飞艇副气 囊的容积;  a determining module, configured to determine, according to the target curved surface, a volume of an airbag sub airbag to which the target surface belongs;
第三获取模块, 用于获取预设的安全容积范围; 报警模块, 用于在所述飞艇副气囊的容积不处于所述安全容积范围的 情况下, 发出报警信号。  And a third obtaining module, configured to obtain a preset safety volume range; and an alarm module, configured to send an alarm signal if the volume of the airship sub-airbag is not within the safe volume range.
[权利要求 14] 一种获取目标曲面的系统, 其特征在于, 包括: [Claim 14] A system for acquiring a target curved surface, comprising:
两台预设光源, 用于发出的出射光线;  Two preset light sources for emitting outgoing light;
图像采集设备, 用于采集由所述出射光线投射在目标曲面上而产生的 图像, 所述图像包括: 多个亮条纹, 所述目标曲面为飞艇副气囊的表 面;  An image capturing device, configured to collect an image generated by the emitted light being projected on a target curved surface, the image comprising: a plurality of bright stripes, wherein the target curved surface is a surface of an airship sub-airbag;
处理器, 与所述图像采集设备相连, 用于从所述图像中的亮条纹上取 多个目标点; 获取所述多个目标点的坐标值, 根据所述多个目标点的 坐标值获取所述目标曲面; 并根据所述目标曲面确定所述飞艇副气囊 的容积。  a processor, connected to the image capturing device, configured to take a plurality of target points from the bright stripe in the image; acquire coordinate values of the plurality of target points, and obtain according to coordinate values of the plurality of target points Determining a volume of the airship sub-airbag according to the target curved surface;
[权利要求 15] 根据权利要求 14所述的系统, 其特征在于, 所述系统还包括: 所述两 台预设光源设置于所述目标曲面前方, 并与所述目标曲面间隔预设距 离。  The system according to claim 14, wherein the system further comprises: the two preset light sources are disposed in front of the target curved surface and spaced apart from the target curved surface by a preset distance.
PCT/CN2017/091951 2016-12-20 2017-07-06 Technical field of method, device and system for acquiring target curved surface WO2018113257A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201611187536.4 2016-12-20
CN201611187536.4A CN108205817B (en) 2016-12-20 2016-12-20 Method, device and system for obtaining target curved surface

Publications (1)

Publication Number Publication Date
WO2018113257A1 true WO2018113257A1 (en) 2018-06-28

Family

ID=62604309

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/091951 WO2018113257A1 (en) 2016-12-20 2017-07-06 Technical field of method, device and system for acquiring target curved surface

Country Status (2)

Country Link
CN (1) CN108205817B (en)
WO (1) WO2018113257A1 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5175601A (en) * 1991-10-15 1992-12-29 Electro-Optical Information Systems High-speed 3-D surface measurement surface inspection and reverse-CAD system
US6751344B1 (en) * 1999-05-28 2004-06-15 Champion Orthotic Investments, Inc. Enhanced projector system for machine vision
WO2013091016A1 (en) * 2011-12-23 2013-06-27 Canon Kabushiki Kaisha Structured light system for robust geometry acquisition
CN104034261A (en) * 2014-06-10 2014-09-10 深圳先进技术研究院 Surface normal measurement device and method
CN105674909A (en) * 2015-12-31 2016-06-15 天津市兆瑞测控技术有限公司 Simple high-precision two-dimensional contour measurement method

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070066541A (en) * 2005-12-22 2007-06-27 재단법인 포항산업과학연구원 3 dimensional displacement measurement apparatus of structure using digital image processing and the method thereof
CN101561259A (en) * 2009-04-21 2009-10-21 天津大学 Phase controllable multi-frequency fiber interference fringe projection device
CN103018740B (en) * 2012-07-19 2014-07-16 电子科技大学 InSAR (Interferometric Synthetic Aperture Radar) imaging method based on curved surface projection

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5175601A (en) * 1991-10-15 1992-12-29 Electro-Optical Information Systems High-speed 3-D surface measurement surface inspection and reverse-CAD system
US6751344B1 (en) * 1999-05-28 2004-06-15 Champion Orthotic Investments, Inc. Enhanced projector system for machine vision
WO2013091016A1 (en) * 2011-12-23 2013-06-27 Canon Kabushiki Kaisha Structured light system for robust geometry acquisition
CN104034261A (en) * 2014-06-10 2014-09-10 深圳先进技术研究院 Surface normal measurement device and method
CN105674909A (en) * 2015-12-31 2016-06-15 天津市兆瑞测控技术有限公司 Simple high-precision two-dimensional contour measurement method

Also Published As

Publication number Publication date
CN108205817A (en) 2018-06-26
CN108205817B (en) 2021-11-09

Similar Documents

Publication Publication Date Title
US10401143B2 (en) Method for optically measuring three-dimensional coordinates and controlling a three-dimensional measuring device
US10088296B2 (en) Method for optically measuring three-dimensional coordinates and calibration of a three-dimensional measuring device
CN104173054B (en) Measuring method and measuring device for height of human body based on binocular vision technique
EP1277026B1 (en) Combined stereovision, color 3d digitizing and motion capture system
EP1792282B1 (en) A method for automated 3d imaging
CN106683038B (en) Method and device for generating fire situation map
US20120307046A1 (en) Methods and apparatus for thermographic measurements
BR102017006726A2 (en) AIRCRAFT COLLISION ALERT SYSTEM AND METHOD FOR GENERATING AN ALERT SIGNAL OF A POTENTIAL AIRCRAFT COLLISION
WO2018227576A1 (en) Method and system for detecting ground shape, method for drone landing, and drone
CN106683039B (en) System for generating fire situation map
US9857232B2 (en) Device for non-contact temperature measurement and temperature measurement method
WO2016040271A1 (en) Method for optically measuring three-dimensional coordinates and controlling a three-dimensional measuring device
AU2019353165B2 (en) Optics based multi-dimensional target and multiple object detection and tracking method
CN115597551A (en) Handheld laser-assisted binocular scanning device and method
CN114724104A (en) Method, device, electronic equipment, system and medium for detecting visual recognition distance
CN110702016A (en) Power transmission line icing measurement system and method
WO2018113257A1 (en) Technical field of method, device and system for acquiring target curved surface
Rossi et al. Measurement of the geometric characteristics of a fire front by stereovision techniques on field experiments
CN204944449U (en) Depth data measuring system
JPH05135155A (en) Three-dimensional model constitution device using successive silhouette image
JP2004295813A (en) 3-dimensional figure verification unit
US11195290B2 (en) Apparatus and method for encoding in structured depth camera system
CN105737803B (en) The two-sided battle array stereo mapping system of aviation
JP7028814B2 (en) External shape recognition device, external shape recognition system and external shape recognition method
CN105571496B (en) A kind of live detection electrical apparatus external insulation configuration parameter measuring method

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 17884750

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 17884750

Country of ref document: EP

Kind code of ref document: A1