CN114623726A - Control method and device for electronic sighting telescope, electronic sighting telescope and storage medium - Google Patents
Control method and device for electronic sighting telescope, electronic sighting telescope and storage medium Download PDFInfo
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/46—Sighting devices for particular applications
- F41G1/473—Sighting devices for particular applications for lead-indicating or range-finding, e.g. for use with rifles or shotguns
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G11/00—Details of sighting or aiming apparatus; Accessories
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/06—Aiming or laying means with rangefinder
- F41G3/065—Structural association of sighting-devices with laser telemeters
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/08—Aiming or laying means with means for compensating for speed, direction, temperature, pressure, or humidity of the atmosphere
Abstract
The invention discloses a control method and a control device for an electronic sighting telescope, the electronic sighting telescope and a storage medium, wherein the method comprises the following steps: when an aiming instruction is received, a laser signal with a preset wavelength is sent to a target object, so that the measuring distance of the target object is determined according to the laser signal; judging whether the measured distance reaches a preset threshold value or not; when the measured distance reaches a preset threshold value, determining current wind power data so as to calculate a wind deviation value according to the wind power data and the measured distance; and generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying. Therefore, when the device is influenced by wind power, auxiliary aiming can be accurately provided, and the aiming accuracy of the target object is improved.
Description
Technical Field
The invention relates to the technical field of sighting telescope, in particular to a control method and device of an electronic sighting telescope, the electronic sighting telescope and a storage medium.
Background
In the field of firearms, a sighting telescope is an important appliance for determining a shooting point, an electronic sighting telescope can process an image into a digital signal, a bullet can be guided by measuring and calculating the digital signal, and the electronic sighting telescope is very wide in application in the field of firearms due to the fact that the electronic sighting telescope is convenient to use and high in hit rate. In the related art, the current electronic sighting telescope can clearly see and identify a target at a far distance and provide distance measurement data to assist the accurate shooting at the far distance, but cannot more accurately provide auxiliary aiming when being influenced by wind power, so that the accuracy of hitting the target is insufficient.
Disclosure of Invention
In a first aspect, the present invention provides a method for controlling an electronic scope, including:
when an aiming instruction is received, a laser signal with a preset wavelength is sent to a target object, so that the measuring distance of the target object is determined according to the laser signal;
judging whether the measured distance reaches a preset threshold value or not;
when the measured distance reaches a preset threshold value, determining current wind power data so as to calculate a wind deviation value according to the wind power data and the measured distance;
and generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying.
Optionally, the emitting a laser signal with a preset wavelength to a target object when receiving the aiming instruction, so as to determine the measured distance of the target object according to the laser signal includes:
when an aiming instruction is received, responding to an operation instruction to output the laser signal with the preset wavelength to the target object; wherein the predetermined wavelength is 625-640 nm;
receiving the laser signal reflected by the target object to determine the conduction time of the laser signal;
and determining the determination distance of the target object according to the conduction time.
Optionally, when the measured distance reaches a preset threshold, determining current wind power data to calculate a wind offset value according to the wind power data and the measured distance includes:
when the measured distance reaches a preset threshold value, acquiring current wind power data based on a wind direction sensor; the wind data comprises wind speed and wind direction;
and calculating the wind deviation value according to the wind direction speed and the measuring distance.
Optionally, the generating a corresponding first visual identifier according to the wind bias value and the measured distance to output the first visual identifier to a display element for displaying includes:
determining a corresponding correction angle and a corresponding correction distance according to the wind deviation value and the wind direction;
generating a corresponding calibration point, an aiming point and a direction deviation rectifying mark according to the correction angle and the correction distance; wherein the direction deviation rectifying mark is opposite to the wind direction;
and outputting the calibration point, the aiming point and the direction deviation rectifying mark to a display element for displaying.
Optionally, the method further comprises:
responding to a deviation rectifying operation instruction of a user, and judging whether the calibration point is overlapped with the aiming point or not;
when the calibration point is overlapped with the aiming point, determining to obtain a target aiming point;
and when the calibration point is not overlapped with the aiming point, generating a new calibration point and a new direction deviation rectifying mark according to the correction angle and the correction distance again.
Optionally, the determining whether the measured distance reaches a preset threshold includes:
when the measured distance does not reach a preset threshold value, determining a corresponding second visual identifier according to the measured distance; wherein the second visual identification comprises an aiming point and a distance identification;
outputting the second visual identification to the display element for display.
In a second aspect, an embodiment of the present invention provides a control device for an electronic sighting telescope, including:
the device comprises a sending module, a detection module and a control module, wherein the sending module is used for sending a laser signal with a preset wavelength to a target object when receiving an aiming instruction so as to determine the measuring distance of the target object according to the laser signal;
the judging module is used for judging whether the measured distance reaches a preset threshold value;
the determining module is used for determining current wind power data when the measured distance reaches a preset threshold value so as to calculate a wind deviation value according to the wind power data and the measured distance;
and the generating module is used for generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying.
Optionally, the sending module includes:
the output unit is used for responding to an operation instruction to output the laser signal with the preset wavelength to the target object when receiving the aiming instruction; wherein the predetermined wavelength is 625-640 nm;
the receiving unit is used for receiving the laser signal reflected by the target object so as to determine the conduction time of the laser signal;
and the determining unit is used for determining the measuring distance of the target object according to the conduction time.
In a third aspect, an embodiment of the present invention provides an electronic sighting telescope, including a memory, a processor, and a control program stored in the memory and executable on the processor, where the processor executes the control program to implement the steps of the control method of the electronic sighting telescope.
In a fourth aspect, an embodiment of the present invention provides a computer-readable storage medium, which stores a control program, and the control program, when executed by a processor, implements the steps of the control method of the electronic scope as described above.
The scheme of the invention at least comprises the following beneficial effects:
the control method of the electronic sighting telescope provided by the invention comprises the steps of sending a laser signal with a preset wavelength to a target object when a sighting instruction is received, and determining the measuring distance of the target object according to the laser signal; judging whether the measured distance reaches a preset threshold value or not; when the measured distance reaches a preset threshold value, determining current wind power data so as to calculate a wind deviation value according to the wind power data and the measured distance; and finally, generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying. Therefore, when the target is influenced by wind power, auxiliary aiming can be accurately provided, and the aiming accuracy of the target is improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is a schematic overall flow chart of a control method of an electronic sighting telescope according to an embodiment of the present invention;
fig. 2 is a schematic flowchart of step S20 according to an embodiment of the present invention;
fig. 3 is a schematic flowchart of step S30 according to an embodiment of the present invention;
fig. 4 is a schematic flowchart of step S40 according to an embodiment of the present invention;
fig. 5 is an exemplary diagram of a control method of an electronic sighting telescope according to an embodiment of the present invention;
FIG. 6 is another schematic flow chart illustrating a method for controlling an electronic sighting telescope according to an embodiment of the present invention;
fig. 7 is a block diagram of an electronic sighting telescope provided in the embodiment of the present invention;
fig. 8 is a block diagram of a sending module according to an embodiment of the present invention;
fig. 9 is a block diagram of an electronic sighting telescope provided in the embodiment of the present invention.
The implementation, functional features and advantages of the present invention will be further described with reference to the accompanying drawings.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The terms "first," "second," and "third," etc. in the description and claims of the present invention and the above-described drawings are used for distinguishing between different objects and not for describing a particular order. Furthermore, the terms "comprises" and any variations thereof, are intended to cover non-exclusive inclusions. For example, a process, method, system, article, or apparatus that comprises a list of steps or elements is not limited to only those steps or elements listed, but may alternatively include other steps or elements not listed, or inherent to such process, method, article, or apparatus.
The following embodiments of the present application will be described by way of example with reference to the accompanying drawings.
As shown in fig. 1, an embodiment of the present invention provides a method for controlling an electronic scope, including:
and S10, when the aiming instruction is received, sending a laser signal with a preset wavelength to the target object so as to determine the measured distance of the target object according to the laser signal.
In this embodiment, the aiming instruction may be sent by a user through a control key or the like, the laser signal may be visible light, and the laser signal may be sent by a photodiode, a laser tube or the like, after the laser signal is sent to the target object, the target object may reflect the laser signal, and may receive the reflected laser signal through a sensor, thereby determining the measurement distance of the target object; it can be understood that the conduction speed of the laser signal is fixed, so that the distance of the target object can be determined by calculating the conduction time of the emitting and receiving of the laser signal.
As shown in fig. 2, the emitting a laser signal with a preset wavelength to the target object when receiving the aiming instruction to determine the measured distance of the target object according to the laser signal includes:
s11, when the aiming instruction is received, responding to the operation instruction and outputting a laser signal with a preset wavelength to the target object; wherein the predetermined wavelength is 625-640 nm;
s12, receiving the laser signal reflected by the target object to determine the conduction time of the laser signal;
and S13, determining the measuring distance of the target object according to the conduction time.
The aiming instruction can be received and responded by the single chip microcomputer, when the aiming instruction is received, a laser signal can be sent to a target object through a laser tube and the like, after the sensor receives the reflected laser signal, the conduction time of the laser signal can be determined through the phase difference of the laser signal, and the distance of the target object is calculated through the conduction time; alternatively, the formula may be calculated by the distance of light
Calculating the measuring distance of the target object, wherein l is the measuring distance of the target object, c is the light speed, and t is the conduction time; alternatively, the laser signal may be visible light, so the preset wavelength may also be 630nm, and the distance measurement is performed by the laser signal pair, so that the measured distance of the target object can be accurately determined in the aiming process, and the accuracy can be adjusted by the measured distance of the target object, so that the operation is simpler in the aiming process.
And S20, judging whether the measured distance reaches a preset threshold value.
In this embodiment, the preset threshold may be 110 meters, and since the device such as a firearm needs to measure the wind power data when the shooting distance is greater than 110 meters, the measured distance may be compared with the preset threshold after the measured distance is determined, whether the measured distance of the target object is greater than the preset threshold may be determined after the comparison, and when the measured distance is greater than the preset threshold, it indicates that the aiming point needs to be corrected by measuring the wind power data; when the measured distance is smaller than a preset threshold value, an aiming point can be determined; it is understood that the preset threshold may be set for a corresponding device, for example, the preset threshold may be set to 110 meters for a firearm-like device, and the preset threshold may be set to 30 meters for a bow-crossbow-like device, so that the device may be applied to different scenes and devices, and the application range is wider.
And S30, when the measured distance reaches a preset threshold value, determining the current wind power data so as to calculate a wind offset value according to the wind power data and the measured distance.
In this embodiment, when the measured distance reaches a preset threshold, it indicates that the measured distance of the target object is affected by wind power, so that a wind deflection value can be calculated by determining wind power data, where the wind power data includes wind speed and wind direction, the wind direction may have cross wind direction, oblique wind direction, and the like, and the wind deflection value may be represented as a wind deflection angle, and when it is determined that the measured distance reaches the preset threshold, it may determine current wind speed and wind direction by using a wind direction sensor, so as to correct and calibrate the aiming point according to the wind speed and the wind direction; it can be understood that the wind data can be obtained by the wind sensor in real time, and the obtained wind data can be output to the single chip microcomputer to calculate the wind offset value.
As shown in fig. 3, the determining the current wind power data when the measured distance reaches the preset threshold value to calculate the wind offset value according to the wind power data and the measured distance includes:
s31, when the measured distance reaches a preset threshold value, acquiring current wind data based on a wind direction sensor; the wind data includes wind speed and wind direction;
and S32, calculating an air outlet deviation value according to the wind direction speed and the measuring distance.
When calculating the wind bias value, the following formula can be adopted for calculation:
Wil/100 xs/k, wherein WiThe method comprises the following steps of (1) expressing a wind deflection value, l expressing a measured distance of a target object, s expressing a wind speed, and k expressing a constant, and correcting an aiming point through the wind deflection value after calculating the wind deflection value so that the aiming point can be adjusted more accurately; therefore, after the windage yaw value is calculated through the windage speed and the measured distance, the current deviation position of the aiming point can be determined through the windage yaw value, and then the aiming point is corrected and calibrated.
And S40, generating a corresponding first visual identifier according to the wind deviation value and the measured distance, and outputting the first visual identifier to a display element for displaying.
As shown in fig. 4, the first visual identifier may include a calibration point, an aiming point and a direction deviation-correcting mark, the calibration point is represented as a point to be aligned, the aiming point is a preset aiming center point, the direction deviation-correcting mark may be a direction arrow, and the display element may be a display screen or the like; the first visual identification is determined and output to the display element to be displayed, so that a user can correct and calibrate according to the first visual identification; it can be understood that the calibration point and the direction deviation correction mark can be determined by the trajectory of a firearm or other equipment; for example, when the aiming point overlaps the target, the aiming point needs to be moved to a position not completely overlapping the target due to wind influence, the corresponding calibration point may be located at the position where the aiming point needs to be moved, and the aiming point may be calibrated by the calibration point.
As shown in fig. 5, the generating a corresponding first visual marker according to the wind drift value and the measured distance to output the first visual marker to a display element for display includes:
s41, determining a corresponding correction angle and a correction distance according to the windage yaw value and the wind direction;
s42, generating a corresponding calibration point, an aiming point and a direction deviation rectifying mark according to the correction angle and the correction distance; wherein, the direction deviation rectifying mark is opposite to the wind direction;
and S43, outputting the calibration point, the aiming point and the direction deviation-rectifying mark to a display element for display.
The correction angle can be expressed as an angle to be corrected by equipment such as firearms and the like, the correction distance is expressed as a distance to be moved when the corresponding angle is corrected, when the correction angle and the correction distance are determined, the correction angle can be determined according to the wind direction, and the correction distance is determined according to the wind deflection value, for example, when the wind deflection value determined by wind blowing from the 9 o 'clock direction is 2moa, the correction angle is towards the 9 o' clock direction, and the correction distance is 33 mil, so that the calibration point is located at the 9 o 'clock direction, the direction deviation correction mark is towards the 9 o' clock direction, and the length corresponds to the correction distance, therefore, after the calibration point, the calibration point and the direction deviation correction mark are determined, the calibration point and the direction deviation correction mark can be jointly output to a display element for a user to check deviation correction and perform operation.
The control method of the electronic sighting telescope provided by the invention comprises the steps of sending a laser signal with a preset wavelength to a target object when a sighting instruction is received, and determining the measuring distance of the target object according to the laser signal; judging whether the measured distance reaches a preset threshold value or not; when the measured distance reaches a preset threshold value, determining current wind power data to obtain a wind deviation value through calculation according to the wind power data and the measured distance; and finally, generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying. Therefore, when the device is influenced by wind power, auxiliary aiming can be accurately provided, and the aiming accuracy of the target object is improved.
As shown in fig. 6, the method for controlling an electronic scope according to the present invention further includes:
51. responding to a deviation rectifying operation instruction of a user, and judging whether the calibration point is overlapped with the aiming point or not;
52. when the calibration point is overlapped with the aiming point, determining to obtain a target aiming point;
53. and when the calibration point is not overlapped with the aiming point, generating a new calibration point and a new direction deviation correction mark according to the correction angle and the correction distance.
In this embodiment, the deviation rectifying operation instruction of the user may be a moving operation instruction of a device such as a firearm, so that when it is determined whether the calibration point overlaps with the aiming point, the electronic sighting telescope may sense through a tilt sensor on the electronic sighting telescope to determine whether the aiming point is moved to a position overlapping with the calibration point, and after the aiming point is moved to overlap with the calibration point, the aiming point may be determined as a target aiming point for shooting; when the calibration point does not overlap with the aiming point after moving, the calibration point and the direction deviation correction mark can be updated according to the windage yaw value determined by real-time detection, so that a user can move equipment such as firearms and the like through the calibration point and the direction deviation correction mark which are updated in real time until the aiming point overlaps with the calibration point to shoot.
Optionally, the determining whether the measured distance reaches the preset threshold includes:
step one, when the measured distance does not reach a preset threshold value, determining a corresponding second visual identifier according to the measured distance; wherein the second visual identification comprises an aiming point and a distance identification;
and step two, outputting the second visual identification to a display element for displaying.
In this embodiment, the distance identifier corresponding to the measured distance may be generated and output to the display element for display, and through the aiming point and the distance identifier, the user may determine the distance to the target object more intuitively when using the device, and through the aiming point, the user may hit the target object more accurately when shooting; it can be understood that, since the measured distance is lower than the preset threshold, it means that the distance of the target object is relatively close and is not easily affected by wind, and therefore, the generated aiming point is not easy to generate errors and has higher accuracy in the shooting process.
As shown in fig. 7, an embodiment of the present invention provides a control device 10 for an electronic scope, including:
the sending module 11 is configured to send a laser signal with a preset wavelength to the target object when receiving the aiming instruction, so as to determine a measurement distance of the target object according to the laser signal;
the judging module 12 is used for judging whether the measured distance reaches a preset threshold value;
the determining module 13 is configured to determine current wind power data when the measured distance reaches a preset threshold value, so as to calculate a wind deviation value according to the wind power data and the measured distance;
and the generating module 14 is configured to generate a corresponding first visual identifier according to the wind deviation value and the measured distance, so as to output the first visual identifier to a display element for displaying.
As shown in fig. 8, the sending module 11 includes:
the output unit 111 is used for responding to the operation instruction to output a laser signal with a preset wavelength to the target object when receiving the aiming instruction; wherein the predetermined wavelength is 625-640 nm;
a receiving unit 112, configured to receive a laser signal reflected by the target object to determine a propagation time of the laser signal;
a determining unit 113 for determining the measured distance of the target object according to the transit time.
The control device 10 of the electronic sighting telescope provided by the invention sends a laser signal with a preset wavelength to a target object when receiving a sighting instruction so as to determine the measuring distance of the target object according to the laser signal; judging whether the measured distance reaches a preset threshold value or not; when the measured distance reaches a preset threshold value, determining current wind power data so as to calculate a wind deviation value according to the wind power data and the measured distance; and finally, generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying. Therefore, when the target is influenced by wind power, auxiliary aiming can be accurately provided, and the aiming accuracy of the target is improved.
It should be noted that the control device 10 of the electronic telescope provided in the specific embodiment of the present invention is a device corresponding to the control method of the electronic telescope, all embodiments of the control method of the electronic telescope are applicable to the control device 10 of the electronic telescope, and corresponding modules in the embodiment of the control device 10 of the electronic telescope correspond to steps in the control method of the electronic telescope, so as to achieve the same or similar beneficial effects, and in order to avoid too many repetitions, each module in the control device 2 of the electronic telescope is not described in detail herein.
As shown in fig. 9, the embodiment of the present invention further provides an electronic sighting telescope 20, which includes a memory 202, a processor 201, and a control program stored in the memory 202 and executable on the processor 201, wherein the processor 201 implements the steps of the control method of the electronic sighting telescope described above when executing the control program.
Specifically, the processor 201 is configured to call the control program stored in the memory 202, and execute the following steps:
when an aiming instruction is received, a laser signal with a preset wavelength is sent to a target object, so that the measuring distance of the target object is determined according to the laser signal;
judging whether the measured distance reaches a preset threshold value or not;
when the measured distance reaches a preset threshold value, determining current wind power data so as to calculate a wind deviation value according to the wind power data and the measured distance;
and generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying.
Optionally, the sending, by the processor 201, a laser signal with a preset wavelength to the target object when the aiming instruction is received, so as to determine the measured distance of the target object according to the laser signal includes:
when an aiming instruction is received, responding to an operation instruction to output the laser signal with the preset wavelength to the target object; wherein the predetermined wavelength is 625-640 nm;
receiving the laser signal reflected by the target object to determine the conduction time of the laser signal;
and determining the determination distance of the target object according to the conduction time.
Optionally, the determining, by the processor 201, current wind data when the measured distance reaches a preset threshold, so as to calculate a wind offset value according to the wind data and the measured distance includes:
when the measured distance reaches a preset threshold value, acquiring current wind power data based on a wind direction sensor; the wind data comprises wind speed and wind direction;
and calculating the wind deviation value according to the wind direction speed and the measuring distance.
Optionally, the generating, by the processor 201, a corresponding first visual identifier according to the wind bias value and the measured distance, so as to output the first visual identifier to a display element for displaying includes:
determining a corresponding correction angle and a corresponding correction distance according to the wind deviation value and the wind direction;
generating a corresponding calibration point, an aiming point and a direction deviation rectifying mark according to the correction angle and the correction distance; wherein the direction deviation rectifying mark is opposite to the wind direction;
and outputting the calibration point, the aiming point and the direction deviation rectifying mark to a display element for displaying.
Optionally, the method for controlling the electronic sighting telescope executed by the processor 201 further includes:
responding to a deviation rectifying operation instruction of a user, and judging whether the calibration point is overlapped with the aiming point or not;
when the calibration point is overlapped with the aiming point, determining to obtain a target aiming point;
and when the calibration point is not overlapped with the aiming point, generating a new calibration point and a new direction deviation rectifying mark according to the correction angle and the correction distance.
Optionally, the determining, executed by the processor 201, whether the measured distance reaches the preset threshold includes:
when the measured distance does not reach a preset threshold value, determining a corresponding second visual identifier according to the measured distance; wherein the second visual identification comprises an aiming point and a distance identification;
outputting the second visual identification to the display element for display.
That is, in the embodiment of the present invention, when the processor 201 of the electronic sighting telescope 20 executes the control program, the steps of the control method of the electronic sighting telescope are implemented, so that auxiliary sighting can be provided more accurately when influenced by wind power, and the sighting accuracy of the target object is improved.
It should be noted that, since the processor 201 of the electronic telescope 20 executes the control program to implement the steps of the control method of the electronic telescope, all the embodiments of the control method of the electronic telescope are applicable to the electronic telescope 20, and the same or similar beneficial effects can be achieved.
The computer-readable storage medium provided in the embodiments of the present invention stores a control program thereon, and the control program, when executed by the processor, implements each process of the control method of the electronic scope or the control method of the application-side electronic scope provided in the embodiments of the present invention, and can achieve the same technical effect, and is not described herein again to avoid repetition.
It will be understood by those skilled in the art that all or part of the processes of the methods of the embodiments described above can be implemented by controlling a program to instruct associated hardware, where the program can be stored in a computer-readable storage medium, and when executed, the program can include the processes of the embodiments of the methods described above. The storage medium may be a magnetic disk, an optical disk, a Read-Only Memory (ROM), a Random Access Memory (RAM), or the like.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the scope of the present invention, and all modifications and equivalents of the present invention, which are made by the contents of the present specification and the accompanying drawings, or directly/indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (10)
1. A method of controlling an electronic scope, comprising:
when an aiming instruction is received, a laser signal with a preset wavelength is sent to a target object, so that the measuring distance of the target object is determined according to the laser signal;
judging whether the measured distance reaches a preset threshold value or not;
when the measured distance reaches a preset threshold value, determining current wind power data so as to calculate a wind deviation value according to the wind power data and the measured distance;
and generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying.
2. The method for controlling an electronic sighting telescope according to claim 1, wherein the step of emitting a laser signal with a preset wavelength to a target object upon receiving a sighting instruction to determine the measured distance of the target object according to the laser signal comprises:
when an aiming instruction is received, responding to an operation instruction to output the laser signal with the preset wavelength to the target object; wherein the predetermined wavelength is 625-640 nm;
receiving the laser signal reflected by the target object to determine the conduction time of the laser signal;
and determining the determination distance of the target object according to the conduction time.
3. The method for controlling an electronic sighting telescope according to claim 1, wherein the determining current wind power data when the measured distance reaches a preset threshold value to calculate a wind offset value from the wind power data and the measured distance comprises:
when the measured distance reaches a preset threshold value, acquiring current wind power data based on a wind direction sensor; the wind data comprises wind speed and wind direction;
and calculating the wind deviation value according to the wind direction speed and the measuring distance.
4. The method of controlling an electronic scope according to claim 3, wherein the generating a corresponding first visual marker from the wind bias value and the measured distance to output the first visual marker to a display element for display comprises:
determining a corresponding correction angle and a corresponding correction distance according to the wind deviation value and the wind direction;
generating a corresponding calibration point, an aiming point and a direction deviation rectifying mark according to the correction angle and the correction distance; wherein, the direction deviation rectifying mark is opposite to the wind direction;
and outputting the calibration point, the aiming point and the direction deviation rectifying mark to a display element for displaying.
5. The method of controlling an electronic sight of claim 4, further comprising:
responding to a deviation rectifying operation instruction of a user, and judging whether the calibration point is overlapped with the aiming point or not;
when the calibration point is overlapped with the aiming point, determining to obtain a target aiming point;
and when the calibration point is not overlapped with the aiming point, generating a new calibration point and a new direction deviation rectifying mark according to the correction angle and the correction distance.
6. The method for controlling an electronic scope according to claim 1, wherein the determining whether the measured distance reaches a preset threshold value comprises:
when the measured distance does not reach a preset threshold value, determining a corresponding second visual identifier according to the measured distance; wherein the second visual identification comprises an aiming point and a distance identification;
outputting the second visual identification to the display element for display.
7. A control device for an electronic scope, comprising:
the device comprises a sending module, a detection module and a control module, wherein the sending module is used for sending a laser signal with a preset wavelength to a target object when receiving an aiming instruction so as to determine the measuring distance of the target object according to the laser signal;
the judging module is used for judging whether the measured distance reaches a preset threshold value;
the determining module is used for determining current wind power data when the measured distance reaches a preset threshold value so as to calculate a wind deviation value according to the wind power data and the measured distance;
and the generating module is used for generating a corresponding first visual identifier according to the wind deviation value and the measured distance so as to output the first visual identifier to a display element for displaying.
8. The control device of an electronic sighting telescope according to claim 7, wherein the transmission module comprises:
the output unit is used for responding to an operation instruction to output the laser signal with the preset wavelength to the target object when receiving the aiming instruction; wherein the predetermined wavelength is 625-640 nm;
the receiving unit is used for receiving the laser signal reflected by the target object so as to determine the conduction time of the laser signal;
and the determining unit is used for determining the measuring distance of the target object according to the conduction time.
9. An electronic sighting telescope comprising a memory, a processor and a control program stored in the memory and executable on the processor, characterized in that the processor implements the steps of the method for controlling an electronic sighting telescope according to any one of claims 1 to 6 when executing the control program.
10. A computer-readable storage medium storing a control program, characterized in that the control program, when executed by a processor, realizes the steps of the control method of an electronic scope according to any one of claims 1 to 6.
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| CN202210054270.5A CN114623726A (en) | 2022-01-18 | 2022-01-18 | Control method and device for electronic sighting telescope, electronic sighting telescope and storage medium |
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| CN202210054270.5A CN114623726A (en) | 2022-01-18 | 2022-01-18 | Control method and device for electronic sighting telescope, electronic sighting telescope and storage medium |
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