Performance test system of strong light dazzler

Abstract

The utility model discloses a performance test system for a hard light dazzler, which comprises an application environment simulation assembly, an application state simulation assembly, an acquisition assembly and a control assembly, and is characterized in that the application environment simulation assembly is configured to be connected with the control assembly and can generate different environment background brightness in a test area; the application state simulation assembly is arranged in the test area, is configured to be connected with the control assembly, and can bear the tested sample and drive the tested sample to rotate and / or lift; the acquisition assembly is arranged corresponding to the application state simulation assembly, is configured to be connected with the control assembly, and can acquire optical parameters and / or azimuth parameters of the tested sample carried by the application state simulation assembly; the control assembly is configured to be connected with the application environment simulation assembly, the application state simulation assembly and the acquisition assembly, and the system can enable the dazzler to highly simulate a first-line actual combat disposal scene, and conveniently, rapidly and precisely complete the test of the dazzling performance of the dazzler.

Description

Technical Field

[0001] The utility model relates to the technical field of police equipment detection, in particular to a performance testing system for a strong light dazzler. Background Art

[0002] A glare dazzler is a directed energy non-lethal weapon and one of the essential weapons for the police or military to control riots and maintain social order. Compared with coherent light sources (lasers), glare dazzlers are mainly equipment that uses wide-spectrum incoherent light sources to emit high-intensity visible light radiation, which passes through the human eyeball and reaches the retina to produce photochemical and thermal effects, causing temporary disturbances in recoverable visual function or a significant decrease in visual resolution. Due to the particularity of its target, which is mainly the sensitive and fragile eyes, safety is equally important while ensuring effectiveness. Therefore, it is increasingly important to comprehensively evaluate the dazzling performance of glare dazzlers.

[0003] At present, the detection of glare dazzlers mainly emphasizes the influence of the isolated parameters of the dazzler itself. However, studies have found that the dazzling performance of glare dazzlers is not only related to the parameters of the dazzler itself, but also closely related to the optical environment conditions and geometric space of the treatment scene.

[0004] Since the performance test of the existing glare dazzler is to collect parameters of the light source of the glare dazzler through a glare tester, the influence of the optical environment conditions and geometric space of the glare dazzler treatment scene is not taken into consideration, resulting in low accuracy of the test results.

[0005] It can be seen that providing a performance testing system for a dazzler with high accuracy is an urgent problem to be solved in the art. Utility Model Content

[0006] In view of the problem of low accuracy in the existing dazzler performance tests, the purpose of the utility model is to provide a performance testing system for a strong light dazzler. By adopting application environment simulation components, application status simulation components and acquisition components, the dazzler can highly simulate a variety of front-line actual combat handling scenarios, and complete the test of the dazzler performance conveniently, quickly and with high precision.

[0007] In order to achieve the above-mentioned purpose, the performance test system of the glare dazzler provided by the utility model includes an application environment simulation component, an application state simulation component, a collection component and a control component.

[0008] The application environment simulation component is configured to be connected to the control component and can generate different environmental background brightness in the test area;

[0009] The application state simulation component is disposed in the test area and is configured to be connected to the control component, and is capable of carrying the sample to be tested and driving the sample to be tested to rotate and / or move up and down;

[0010] The acquisition component is arranged corresponding to the application state simulation component, configured to be connected to the control component, and capable of acquiring optical parameters and / or orientation parameters of the sample under test carried by the application state simulation component;

[0011] The control component is configured to connect the application environment simulation component, the application state simulation component and the collection component.

[0012] Furthermore, the application environment simulation component is composed of a light box component with adjustable background brightness.

[0013] Furthermore, a light-homogenizing screen is provided on the light box assembly.

[0014] Furthermore, the light-homogenizing screen is composed of a light guide plate and a light-homogenizing film.

[0015] Furthermore, the light box assembly includes a reflective bottom plate and an array light source group arranged on the reflective bottom plate.

[0016] Furthermore, the application state simulation component is composed of a multi-axis gimbal component.

[0017] Furthermore, the multi-axis pan-tilt head assembly includes a lifting base, a rotating platform and a flexible sample holder. The rotating platform is arranged on the lifting base, and the flexible sample holder is placed on the rotating platform.

[0018] Furthermore, the flexible sample holder is composed of an adjustable clamping frame.

[0019] Furthermore, the acquisition component includes a multi-axis pan-tilt platform, a glare tester, and a laser-assisted locator. The glare tester and the laser-assisted locator are placed on the multi-axis pan-tilt platform and are respectively connected to the control component.

[0020] Furthermore, the control component is composed of a data processing terminal and at least one controller, the data processing terminal is connected to the controller, and the controller is connected to the application environment simulation component, the application state simulation component and the acquisition component.

[0021] The performance testing system of the strong light dazzler provided by the utility model adopts an application environment simulation component to highly simulate the optical environment conditions in different handling scenarios encountered in actual combat, and then presets the rotation angle of the dazzler according to needs through the application state simulation component to complete the adjustment of the angle in the horizontal direction of the dazzler to test the dazzling performance of the dazzler at different angles. Finally, the acquisition component collects light parameters of the light intensity value of the dazzler, which greatly improves the accuracy and reliability of the performance test. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] The present invention is further described below in conjunction with the accompanying drawings and specific implementations.

[0023] Figure 1 The overall structural diagram of the performance test system of the strong light dazzler provided by the utility model;

[0024] Figure 2 A schematic diagram of the structure of the application environment simulation component in the performance test system of the strong light dazzler provided by the utility model;

[0025] Figure 3 A structural schematic diagram of an application state simulation component in a performance test system of a strong light dazzler provided by the utility model;

[0026] Figure 4 This is a structural schematic diagram of a collection component in a performance test system of a strong light dazzler provided by the utility model.

[0027] Illustration Description:

[0028] Application environment simulation component 100, application state simulation component 200, collection component 300, control component 400;

[0029] Array light box 110, box body 111, heat dissipation holes 111a, array LED light group 112, reflective bottom plate 120, light-distributing screen 130, light guide plate 131, light-distributing film 132, shading plate 140, heat dissipation assembly 150, lifting base 210, rotating platform 220, flexible sample holder 230, clamping holder 231, bidirectional screw 232, multi-axis gimbal 310, first drive assembly 311, second drive assembly 312, third drive assembly 313, laser-assisted locator 320, glare tester 330, mounting assembly 340, data processing terminal 410, first controller 421, second controller 422. DETAILED DESCRIPTION

[0030] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below with reference to specific illustrations.

[0031] Embodiment 1:

[0032] See also Figure 1 , which is a structural schematic diagram of the performance testing system of the strong light dazzler provided by the utility model.

[0033] According to the figure, it can be known that the performance test system of the glare dazzler provided by the utility model includes four components: an application environment simulation component 100, an application state simulation component 200, a collection component 300 and a control component 400.

[0034] The performance test system of the strong light dazzler provided by the utility model is applied to the dazzler to test the dazzling performance of the dazzler, which can make the dazzler highly simulate the front-line actual combat handling scene, improve the scientificity and fairness of the test, and greatly improve the accuracy of the test result.

[0035] Wherein, the application environment simulation component 100 is configured to be connected to the control component 400 and can generate different environmental background brightness in the test area;

[0036] The application state simulation component 200 is disposed in the test area and is configured to be connected to the control component 400, and is capable of carrying the tested sample and driving the tested sample to rotate and / or move up and down in the test area;

[0037] The acquisition component 300 is provided corresponding to the above-mentioned application state simulation component 200, and is configured to be connected to the control component 400, and can acquire the optical parameters and / or orientation parameters of the sample carried by the application state simulation component 200;

[0038] The control component 400 is configured to connect the application environment simulation component 100 , the application state simulation component 200 and the collection component 300 .

[0039] The above-mentioned tested sample in this example uses a dazzler, which is only an example for illustration and does not constitute a limitation to this solution.

[0040] In actual application, the dazzler is fixed on the application state simulation component 200, and the application state simulation component 200 adjusts the vertical height of the dazzler up and down according to the size and height of the dazzler. Then, the rotation angle is preset as needed to complete the adjustment of the horizontal angle of the dazzler. In this way, the dazzling performance of the dazzler at different angles can be tested, and then the optical environment conditions in different handling scenarios encountered in actual combat can be highly simulated through the application environment simulation component 100. Finally, the collection component 300 collects the optical parameters and / or orientation parameters of the dazzler by moving.

[0041] Specifically, Figure 2 , the application environment simulation component 100 is composed of a light box component with adjustable background brightness;

[0042] The light box assembly is connected to the control assembly 400 , and the brightness of the light source of the light box assembly can be freely adjusted through the control of the control assembly 400 .

[0043] Furthermore, a light-evening screen 130 is provided on the light box assembly, and the light-evening screen 130 covers a side of the light box assembly where the light source is provided.

[0044] The above-mentioned light-homogenizing screen 130 has the function of diffusing light, so that the light is scattered through the surface, thereby playing a light-homogenizing role, making the light display more uniform and soft;

[0045] Furthermore, the light-homogenizing screen 130 is composed of a light guide plate 131 and a light-homogenizing film 132. The light guide plate 131 is adapted to the light box assembly. The first surface of the light guide plate 131 covers the light box assembly, and the light-homogenizing film 132 covers the second surface of the light guide plate 131.

[0046] The light transmittance of the above-mentioned uniform light screen 130 is preferably greater than or equal to 70%, and the haze is preferably greater than or equal to 90%.

[0047] Specifically, the light box assembly includes a reflective bottom plate 120 and an array light source group 110 disposed on the reflective bottom plate 120 , and a light shielding plate 140 is disposed between the light box assembly and the light-homogenizing screen 130 .

[0048] In some embodiments of the present invention, the array light source group 110 includes a box body 111 and an array LED light group 112;

[0049] A reflective bottom plate 120 is provided on one side of the box body 111, and a placement structure adapted to the display LED light assembly 112 is provided on the reflective bottom plate 120. The reflective bottom plate 120 can accommodate the display LED light assembly 112 to be arranged thereon, and a shading plate 140 is adapted to the reflective bottom plate 120, and the shading plate 140 covers the reflective bottom plate 120 and accommodates the display LED light assembly 112.

[0050] The display LED light assembly 112 is connected to the control assembly 400 , and the brightness of the display LED light assembly 112 is adjusted by the control assembly 400 .

[0051] In this solution, the control component 400 adjusts the brightness by adjusting the optical power of the display LED light assembly 112, so as to highly simulate the optical environment conditions in different handling scenarios encountered in actual combat. For example, the background brightness of the environment on a clear day is 32000 cd / m 2 , the background brightness of daily indoor lighting conditions is 100 cd / m 2 , dark environment background brightness is 0.03cd / m 2 wait.

[0052] In order to further improve the reliability of the light box assembly, the present solution provides a heat dissipation structure for the light box assembly to prevent its temperature from being too high. A plurality of heat dissipation holes 111a are provided on the top of the box body 111. The heat dissipation holes 111a allow the inside of the box body 111 to communicate with the outside world. The hot air generated by the LED light assembly 112 can flow from the heat dissipation holes 111a to the outside world, thereby improving the heat dissipation effect.

[0053] A heat dissipation component 150 is also provided. The heat dissipation component is located at the back of the box body 111 and is used to dissipate heat therefor to avoid the problem of over-temperature caused by long-term operation.

[0054] The present solution does not limit the structure of the heat dissipation assembly 150 , which can be determined according to actual needs. For example, a heat dissipation fan assembly can be used.

[0055] The application environment simulation component 100 of such a structure cooperates with the application state simulation component 200. The application environment simulation component 100 is located next to the application state simulation component 200, and can simulate the dazzler on the application state simulation component 200 to the light brightness during actual application. In this way, when testing the dazzler on the application state simulation component 200, the test result is more accurate and reliable.

[0056] like Figure 3 The application state simulation component 200 is composed of a multi-axis pan-tilt assembly, which is provided with a mounting structure for supporting and fixing the sample to be tested, and can drive the sample to be tested to move in multiple axes, so as to drive the sample to be tested to move vertically and adjust the horizontal angle.

[0057] As an example, Figure 3 , the application state simulation component 200 includes a lifting base 210, a rotating platform 220, and a flexible sample holder 230;

[0058] The lifting shaft of the lifting base 210 is connected to the rotating platform 220. The flexible sample holder 230 is arranged on the rotating platform 220 to fix the sample to be tested. The lifting base 210 and the rotating platform 220 are respectively connected to the control component 400. Through the control of the control component 400, the electric-controlled lifting chassis 210 can be driven to lift vertically and the rotating platform 220 can be driven to rotate axially. The flexible sample holder 230 located on the rotating platform 220 can be driven to achieve vertical height adjustment and axial rotation. Since the sample to be tested is fixed on the flexible sample holder 230, it follows the vertical height adjustment and axial rotation.

[0059] Furthermore, the flexible sample holder 230 in this solution is composed of an adjustable clamping frame. The adjustable clamping frame is used to clamp the sample to be tested, and can also adjust the size of the clamping space to achieve clamping and fixing of samples of different sizes to be tested.

[0060] In some embodiments of the utility model, the adjustable clamping frame includes two clamping brackets 231 and a span adjustment component, which are cooperatively connected to form a clamping space for clamping the dazzler between the two clamping brackets 231. The span adjustment component can adjust the distance between the two flexible sample brackets 230, thereby adjusting the size of the clamping space.

[0061] As an example, the span adjustment assembly includes a bidirectional screw rod 232 and two screw nuts. The bidirectional screw rod 232 is rotatably arranged on the top of the rotating platform 220. The bidirectional screw rod 232 has two left and right sections of external threads with opposite spiral directions. The two screw nuts are respectively screwed on the two sections of external threads with opposite directions. The two screw nuts are respectively connected to two clamping brackets 231. By rotating the bidirectional screw rod 232, the two screw nuts on it can be driven to move relative to each other or move relatively away from each other, thereby adjusting the distance between the two clamping brackets 231 to adapt to dazzlers of various sizes.

[0062] The bidirectional screw rod 232 is preferably connected to the rotating platform 220 via a bearing. The specific structure of the lifting base 210 and the rotating platform 220 is not limited in this embodiment, and is a well-known technology for those skilled in the art, so it will not be described in detail here.

[0063] The application state simulation component 200 of such a structure cooperates with the collection component 300 , and the collection component 300 is located beside the application state simulation component 200 to test the dazzler on the application state simulation component 200 .

[0064] like Figure 4 , the acquisition component 300 includes a multi-axis gimbal 310, a laser-assisted locator 320, and a glare tester 330;

[0065] The laser auxiliary locator 320 and the glare tester 330 are set on the multi-axis pan-tilt head 310 through the mounting component 340, and are respectively connected to the control component 400. Through the control of the control component 400, the multi-axis pan-tilt head 310 can drive the laser auxiliary locator 320 and the glare tester 330 to move in multiple directions to realize the optical parameter and / or azimuth parameter collection of the dazzler.

[0066] The multi-axis gimbal 310 is provided with a first driving assembly 311, a second driving assembly 312, and a third driving assembly 313 for driving;

[0067] The first driving component 311, the second driving component 312, the third driving component 313, the dazzle tester 330, and the laser auxiliary locator 320 are respectively connected to the control component 400. The laser auxiliary locator 320 is used to locate and measure the distance of the dazzler, and can collect azimuth parameters and output them to the control component 400. Through the control of the control component 400, the multi-axis gimbal 310 can drive the laser auxiliary locator 320 and the dazzle tester 330 arranged thereon to move horizontally, horizontally, longitudinally and vertically based on the azimuth parameters of the laser auxiliary locator 320, so that the dazzle tester 330 is adjusted to the maximum light intensity position of the dazzler or to various angles of the dazzler, and collects the light intensity parameters of the dazzler or the light intensity parameters of the dazzler at various angles.

[0068] The laser auxiliary locator 320 has the functions of laser distance measurement and emitting light spots. In actual application, its main function is to assist in the visual determination of the light emission position when installing the dazzler, and to preliminarily determine the approximate position of the center of the light spot. The specific operation is to first install the dazzler on the application state simulation component 200, and then turn on the laser auxiliary locator 320. Through the position adjustment of the multi-axis gimbal 310, the center of the light spot of the laser auxiliary locator 320 is visually overlapped with the center of the light outlet of the dazzler, and the distance measurement is completed. Then, the three-axis mobile platform is fine-tuned according to the measured distance to complete the preliminary auxiliary positioning. This is because due to the different sizes and types of dazzlers, the preset distance may have errors with the actual distance from the dazzler to the lens of the dazzler tester 330, so it is necessary to determine the distance and complete the fine-tuning through the multi-axis gimbal 310;

[0069] Finally, the collection of basic parameters of the glare tester 330 is based on finding the center of the light spot. First, the coordinates of the dazzler at the maximum value are determined, and then the background brightness, effective diameter of the light spot, luminous intensity, beam angle and other parameters of the application environment simulation component 100 are collected in turn. Finally, the rotating platform 220 is rotated at a certain angular velocity to simulate the front-line law enforcement scene.

[0070] The mounting assembly 340 is connected to the multi-axis gimbal 310 , and a connection structure corresponding to the laser auxiliary locator 320 and the glare tester 330 is provided on the mounting assembly 340 , and the laser auxiliary locator 320 and the glare tester 330 are connected to the mounting assembly 340 .

[0071] The present solution does not limit the structure of the multi-axis gimbal 310 , which is a technology well known to those skilled in the art and will not be described in detail here.

[0072] As an example, the multi-axis gimbal 310 may be composed of two parallel X-axis linear modules, a Y-axis linear module, and a Z-axis linear module;

[0073] The two X-axis linear modules have the same structure, both including an X-axis base, and an X-axis screw rotatably arranged in the X-axis base, an X-axis screw nut is provided on the X-axis screw, and an X-axis guide rail is provided on the X-axis base. The X-axis guide rail is used to place the Y-axis linear module, and a first driving component 311 is provided at one end of the X-axis base. The driving shaft of the first driving component 311 is connected to the X-axis screw. Through the drive of the first driving component 311, the X-axis screw can be driven to rotate, and the X-axis screw nut thereon can be driven to move along its straight line.

[0074] The Y-axis linear module includes a Y-axis base, and a Y-axis screw rotatably arranged in the Y-axis base, a Y-axis screw nut is arranged on the Y-axis screw, a Y-axis guide rail is arranged on the Y-axis base, and the Y-axis guide rail is used to place the Z-axis linear module. A second driving component 312 is arranged at one end of the Y-axis base, and the driving shaft of the second driving component 312 is connected to the Y-axis screw. The bottom of the Y-axis base is adapted to the X-axis guide rail. The Y-axis base is movably arranged on the X-axis guide rails of the two X-axis linear modules and connected with the X-axis screw nut. The second driving component 312 can drive the Y-axis screw to rotate and drive the Y-axis screw nut thereon to move along its straight line.

[0075] The Z-axis linear module includes a Z-axis base, and a Z-axis screw rotatably arranged in the Z-axis base, a Z-axis screw nut is provided on the Z-axis screw, and a Z-axis guide rail is provided on the Z-axis base. The Z-axis guide rail is used to place the mounting module 340. One end of the Z-axis base is movably arranged on the Y-axis guide rail and connected to the Y-axis screw nut, and the other end is provided with a third driving component 313. The driving shaft of the third driving component 313 is connected to the Z-axis screw. Through the drive of the third driving component 313, the Z-axis screw can be driven to rotate, and the Z-axis screw nut thereon can be driven to move along its straight line.

[0076] Through the above technical solution, the mounting module 340 is movably set on the Y-axis guide rail of the Y-axis linear module and connected to the Y-axis lead screw nut in the Y-axis base. The laser-assisted positioner 320 and the glare tester 330 are connected to the mounting module 340. Through the drive of the above-mentioned first drive component 311, the second drive component 312, and the third drive component 313, the X-axis lead screw nut, the Y-axis lead screw nut, and the Z-axis lead screw nut are moved linearly, so that the mounting module 340 connected to the Z-axis lead screw nut follows the movement. Due to the motion transmission, the laser-assisted positioner 320 and the glare tester 330 set on the mounting module 340 are moved in the horizontal, longitudinal and vertical directions.

[0077] Furthermore, the control component 400 is composed of a data processing terminal 410 and at least one controller, the data processing terminal 410 is connected to the controller, and the controller is connected to the application environment simulation component 100, the application state simulation component 200 and the acquisition component 300 to control the above components.

[0078] like Figure 1 In this example, the control component 400 uses two controllers, a first controller 421 and a second controller 422. The data processing terminal 410 is connected to the array light source group 110 through the first controller 421, and the data processing terminal 410 is connected to the lifting base 210, the rotating platform 220, the first driving component 311, the second driving component 312, the third driving component 313 and the glare tester 330 in the application state simulation component 200 through the second controller 422.

[0079] Control is performed through the data processing terminal 410, and the first controller 421 and the second controller 422 respectively send corresponding signals to control the brightness of the display LED light assembly 112, the application state simulation assembly 200 performs vertical movement and rotational motion, the multi-axis gimbal 310 performs horizontal, longitudinal and vertical movement, and receives the light parameter data measured by the glare tester 330. The staff can obtain the test results by directly observing at the data processing terminal 410, which can facilitate comparison and recording of the test results.

[0080] The data processing terminal 410 is preferably a mobile computer.

[0081] This solution uses an application environment simulation component 100 to highly simulate the optical environment conditions in different handling scenarios encountered in actual combat, and then uses an application state simulation component 200 to preset the rotation angle of the dazzler as needed to complete the adjustment of the horizontal angle of the dazzler to test the dazzling performance of the dazzler at different angles. Finally, the collection component 300 collects light parameters of the light intensity value of the dazzler by moving, which greatly improves the accuracy and reliability of the performance test.

[0082] Embodiment 2:

[0083] This embodiment describes the structure of the application state simulation component 200 and the multi-axis gimbal 310 based on the embodiment 1. The remaining structures are the same and will not be described in detail here.

[0084] In order to further improve the flexibility of movement of the application state simulation component 200 and the multi-axis pan-tilt platform 310, the structures of the application state simulation component 200 and the multi-axis pan-tilt platform 310 are changed in this example.

[0085] In this example, the application state simulation component 200 and the multi-axis pan-tilt platform 310 can both adopt robot arms. By adopting two robot arms to replace the application state simulation component 200 and the multi-axis pan-tilt platform 310, one of the robot arms can clamp the sample to be tested and drive the sample to be tested to move in multiple directions, and the arm end of the other robot arm is equipped with a laser auxiliary positioner 320 and a glare tester 330. The laser auxiliary positioner 320 and the glare tester 330 are driven by the robot arm to move in multiple directions, so as to realize the collection of optical parameters and / or orientation parameters of the sample to be tested.

[0086] The above-mentioned robot arm is a technology well known to those skilled in the art and will not be described in detail here.

[0087] The above shows and describes the basic principle, main features and advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions are only for explaining the principle of the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the utility model to be protected. The scope of protection of the utility model is defined by the attached claims and their equivalents.

Claims

1. A performance test system for a glare dazzler, characterized in that: Including application environment simulation components, application status simulation components, acquisition components and control components, The application environment simulation component is configured to be connected to the control component and can generate different environmental background brightness in the test area; The application state simulation component is disposed in the test area and is configured to be connected to the control component, and is capable of carrying the sample to be tested and driving the sample to be tested to rotate and / or move up and down; The acquisition component is arranged corresponding to the application state simulation component, configured to be connected to the control component, and capable of acquiring optical parameters and / or orientation parameters of the sample under test carried by the application state simulation component; The control component is configured to connect the application environment simulation component, the application state simulation component and the collection component.

2. The performance test system of the glare dazzler according to claim 1, characterized in that: The application environment simulation component is composed of a light box component with adjustable background brightness.

3. The performance test system of the glare dazzler according to claim 2, characterized in that: The light box assembly is provided with a light-homogenizing screen.

4. The performance test system of the glare dazzler according to claim 3 is characterized in that: The light-homogenizing screen is composed of a light guide plate and a light-homogenizing film.

5. The performance testing system of the glare dazzler according to claim 2, characterized in that: The light box assembly comprises a reflective bottom plate and an array light source group arranged on the reflective bottom plate.

6. The performance test system of the glare dazzler according to claim 1, characterized in that: The application state simulation component is composed of a multi-axis pan-tilt head component.

7. The performance test system of the glare dazzler according to claim 6, characterized in that: The multi-axis pan-tilt platform assembly comprises a lifting base, a rotating platform and a flexible sample holder. The rotating platform is arranged on the lifting base, and the flexible sample holder is placed on the rotating platform.

8. The performance testing system of the glare dazzler according to claim 7, characterized in that: The flexible sample holder is composed of an adjustable clamping frame.

9. The performance test system of the glare dazzler according to claim 1, characterized in that: The acquisition component comprises a multi-axis pan-tilt platform, a dazzle tester and a laser auxiliary locator. The dazzle tester and the laser auxiliary locator are arranged on the multi-axis pan-tilt platform and are respectively connected to the control component.

10. The performance testing system of the glare dazzler according to claim 1, characterized in that: The control component is composed of a data processing terminal and at least one controller. The data processing terminal is connected to the controller. The controller is connected to an application environment simulation component, an application state simulation component and a collection component.

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