CN115291547A - Electric flight-reach detection system and method and electronic equipment - Google Patents
Electric flight-reach detection system and method and electronic equipment Download PDFInfo
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- CN115291547A CN115291547A CN202210928794.2A CN202210928794A CN115291547A CN 115291547 A CN115291547 A CN 115291547A CN 202210928794 A CN202210928794 A CN 202210928794A CN 115291547 A CN115291547 A CN 115291547A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/24—Pc safety
- G05B2219/24215—Scada supervisory control and data acquisition
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Abstract
The present disclosure provides a detection system, a method and an electronic device for electric flight, the system includes: the system comprises a singlechip control module, a flight control module and a flight communication module; the single chip microcomputer control module is connected with the flight control module and the flight communication module; the system comprises a flight control module, a singlechip control module and a communication module, wherein the flight control module is used for generating a flight control signal and sending the flight control signal to the singlechip control module; the single chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module; and the flight communication module is used for sending the flight control instruction to the electric flight so as to enable the electric flight to execute corresponding control operation. Therefore, the control of the electric flight controller is realized through the singlechip control module, and the electric flight controller detects the electric flight controller according to flight controller control signals input by the flight controller. The detection of the electric feeder is integrated in a small single chip microcomputer system, so that the detection of the electric feeder is more convenient, and the detection cost of the electric feeder is reduced.
Description
Technical Field
The invention relates to the field of equipment detection, in particular to a system and a method for detecting an electric flight arrival and electronic equipment.
Background
An electric Feeder is an electric device for industrial feeding and is mainly arranged in a feeding station of each assembly processing line. In general, the number of devices for the electric boomerang is large to meet the processing requirements, and therefore, the routine maintenance and inspection of the electric boomerang becomes an important problem to be faced in each industrial production. In the prior art, the detection of the electric feeder needs larger-sized detection equipment, the detection equipment has larger volume and heavier weight, is inconvenient to transport, move and use, and has higher detection cost when being applied to the electric feeder.
Disclosure of Invention
In view of the above, an object of the present disclosure is to provide a system and a method for detecting an electric femto-controller, and an electronic device, so as to solve the technical problem of inconvenient detection of the electric femto-controller in the related art.
In view of the above object, a first aspect of the present disclosure provides a detection system for an electric femto, the system comprising: the system comprises a singlechip control module, a flight control module and a flight communication module; the single-chip microcomputer control module is connected with the flight control module and the flight communication module;
the system comprises a single-chip microcomputer control module, an access control module and a communication module, wherein the access control module is used for generating an access control signal and sending the access control signal to the single-chip microcomputer control module;
the single chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module;
the flight communication module is used for sending the flight control instruction to the electric flight so as to enable the electric flight to execute corresponding control operation.
Further, the system further comprises: the display module is connected with the single chip microcomputer control module;
the flight communication module can also be used for monitoring the running state information of the electric flight and sending the running state information to the single-chip microcomputer control module;
the single chip microcomputer control module can also be used for sending the running state information to the display module;
and the display module is used for displaying the running state information in the corresponding display area.
Further, the electric femto also comprises an identity barcode, and the system further comprises: the bar code scanning input module is connected with the single chip microcomputer control module;
the bar code scanning input module is used for scanning the identity bar code corresponding to the electric flight platform, generating an identity serial number according to the identity bar code and sending the identity serial number to the single-chip microcomputer control module;
the singlechip control module is used for binding the identity serial number with the electric flight arrival strongly and sending the identity serial number to the display module;
the display module is used for displaying the identity serial number in the display area.
Further, the reach control module comprises: the system comprises a flight arrival power switch unit, a flight arrival reset unit, a first side edge detection unit, a second side edge detection unit, an SN reading unit and an SN input unit;
the flight access power switch unit is used for generating a power supply starting signal and sending the power supply starting signal to the single chip microcomputer control module;
the flight arrival resetting unit is used for generating a resetting signal and sending the resetting signal to the single-chip microcomputer control module;
the first side detection unit is used for generating a first detection control signal corresponding to a first side position of the electric flight reach and sending the first detection control signal to the single chip microcomputer control module;
the second side detection unit is used for generating a second detection control signal of the electric flight reach corresponding to the second side position and sending the second detection control signal to the single chip microcomputer control module;
the SN reading unit is used for reading an SN serial number of the electric flight platform and sending the SN serial number to the single-chip microcomputer control module;
the SN input unit is used for inputting a target SN serial number of the electric flight and sending the target SN serial number to the single-chip microcomputer control module.
Further, the system further comprises: the power input module is connected with the single-chip microcomputer control module;
and the power supply input module is used for inputting electric energy to the single chip microcomputer control module.
Further, the system further comprises: the clock module is connected with the single-chip microcomputer control module;
the clock module is used for generating a clock signal and sending the clock signal to the single chip microcomputer control module.
A second aspect of the present disclosure provides a method for detecting an electric femto, which is applied to the detection system of any one of the first aspect, and includes:
generating a first side control signal of the electric flight in response to a first confirmation operation of a user;
controlling the electric flight path to perform first side operation according to the first side control signal;
and if the first side corresponding to the electric flight reach does not act, generating a fault signal to perform fault early warning.
Further, the method further comprises:
generating a reset signal of the electric flight in response to a second confirmation operation by a user;
and resetting the electric feeder according to the reset signal.
Further, the method further comprises:
acquiring an SN number of the electric Feida;
and controlling the electric flight access to enter a test mode according to the SN number.
A third aspect of the present disclosure provides an electronic device comprising a computer program which, when executed by a processor, implements the steps of the method for detecting an electric femto-sensor in the second aspect described above.
The present disclosure can achieve at least the following advantageous effects:
through above-mentioned scheme, provide a provider's electronic flight and reach detecting system, the system includes: the system comprises a singlechip control module, a flight control module and a flight communication module; the single chip microcomputer control module is connected with the flight control module and the flight communication module; the system comprises a flight control module, a singlechip control module and a communication module, wherein the flight control module is used for generating a flight control signal and sending the flight control signal to the singlechip control module; the single chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module; and the flight communication module is used for sending the flight control instruction to the electric flight so as to enable the electric flight to execute corresponding control operation. Therefore, the control of the electric flight reach is realized through the single-chip microcomputer control module, and the electric flight reach is detected according to the flight reach control signal input by the flight reach control module. The detection of the electric feeder is integrated in a small single chip microcomputer system, so that the detection of the electric feeder is more convenient, and the detection cost of the electric feeder is reduced.
Drawings
FIG. 1 is a block diagram illustrating a detection system for an electric fly-by, according to an exemplary embodiment.
FIG. 2 is an exemplary diagram illustrating another electric femto-detection system in accordance with an exemplary embodiment.
FIG. 3 is a flow chart illustrating a method of detection of an electric fly-by, according to an exemplary embodiment.
FIG. 4 is a block diagram illustrating an electronic device in accordance with an example embodiment.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein, as those skilled in the art will recognize without departing from the spirit and scope of the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one of the feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless explicitly specified otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless otherwise expressly stated or limited, the first feature "on" or "under" the second feature may be directly contacting the first and second features or indirectly contacting the first and second features through an intermediate. Also, a first feature "on," "above," and "over" a second feature may be directly on or obliquely above the second feature, or simply mean that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. As used herein, the terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like are for purposes of illustration only and do not denote a single embodiment.
Fig. 1 is a block diagram illustrating a detection system for an electric femto according to an exemplary embodiment, as shown in fig. 1, the system including: the system comprises a singlechip control module, a flight control module and a flight communication module; the single-chip microcomputer control module is connected with the flight control module and the flight communication module;
the system comprises a single-chip microcomputer control module, an access control module and a communication module, wherein the access control module is used for generating an access control signal and sending the access control signal to the single-chip microcomputer control module;
the single-chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module;
the femto-cell communication module is used for sending the femto-cell control command to the electric femto-cell so as to enable the electric femto-cell to execute corresponding control operation.
Further, the system further comprises: the display module is connected with the single-chip microcomputer control module;
the flight communication module can also be used for monitoring the running state information of the electric flight and sending the running state information to the single-chip microcomputer control module;
the single chip microcomputer control module can also be used for sending the running state information to the display module;
and the display module is used for displaying the running state information in the corresponding display area.
It can be understood that the test system of the electric femto-meter in the embodiment of the present disclosure can be integrated in an electronic device of 160mm × 80cm × 28cm, so as to improve the detection portability of the electric femto-meter and facilitate the detection of the electric femto-meter. The control signal of the electric flight is generated through the single-chip microcomputer control module, the electric flight executes corresponding control operation, and the control operation is compared with the control command in the flight control module, so that whether the corresponding electric flight sends a fault or not is determined. The flight communication module and the electric flight can be connected through wires for signal transmission, and can transmit control instructions to the electric flight in a wireless communication mode.
Further, the electric femto also comprises an identity barcode, and the system further comprises: the bar code scanning input module is connected with the single chip microcomputer control module;
the bar code scanning input module is used for scanning the identity bar code corresponding to the electric flight platform, generating an identity serial number according to the identity bar code and sending the identity serial number to the single-chip microcomputer control module;
the singlechip control module is used for binding the identity serial number with the electric flight arrival strongly and sending the identity serial number to the display module;
the display module is used for displaying the identity serial number in the display area.
Further, the reach control module comprises: the system comprises a femto power switch unit, a femto reset unit, a first side detection unit, a second side detection unit, an SN reading unit and an SN input unit;
the flight access power switch unit is used for generating a power supply starting signal and sending the power supply starting signal to the single chip microcomputer control module;
the flight arrival resetting unit is used for generating a resetting signal and sending the resetting signal to the single chip microcomputer control module;
the first side detection unit is used for generating a first detection control signal corresponding to a first side position of the electric flight reach and sending the first detection control signal to the single-chip microcomputer control module;
the second side detection unit is used for generating a second detection control signal of the electric flight reach corresponding to the second side position and sending the second detection control signal to the single chip microcomputer control module;
the SN reading unit is used for reading an SN serial number of the electric flight platform and sending the SN serial number to the single-chip microcomputer control module;
the SN input unit is used for inputting a target SN serial number of the electric flight and sending the target SN serial number to the single chip microcomputer control module.
Further, the system further comprises: the power input module is connected with the single chip microcomputer control module;
and the power supply input module is used for inputting electric energy to the single chip microcomputer control module.
Further, the system further comprises: the clock module is connected with the single-chip microcomputer control module;
the clock module is used for generating a clock signal and sending the clock signal to the single chip microcomputer control module.
Through above-mentioned scheme, provide a provider's electronic flight and reach detecting system, the system includes: the system comprises a singlechip control module, a flight control module and a flight communication module; the single chip microcomputer control module is connected with the flight control module and the flight communication module; the system comprises a single chip microcomputer control module, an access control module and a communication module, wherein the access control module is used for generating an access control signal and sending the access control signal to the single chip microcomputer control module; the single chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module; and the flight communication module is used for sending the flight control instruction to the electric flight so as to enable the electric flight to execute corresponding control operation. Therefore, the control of the electric flight reach is realized through the single-chip microcomputer control module, and the electric flight reach is detected according to the flight reach control signal input by the flight reach control module. The detection of the electric feeder is integrated in a small single chip microcomputer system, so that the detection of the electric feeder is more convenient, and the detection cost of the electric feeder is reduced.
Fig. 2 is an exemplary diagram illustrating another electric femto detection system according to an exemplary embodiment, where the detection system includes a single-chip CPU, a femto power supply unit, a femto reset unit, a left detection unit, a right detection unit, a stop unit, an SN read unit, an SN write unit, a barcode scan input module, a power input module, a crystal oscillator module, a display, and a femto connection module. Wherein, the singlechip CPU adopts a 32-bit singlechip processor; the system comprises a femto power supply unit, a femto reset unit, a left detection unit, a right detection unit, a stop unit, an SN reading unit and an SN writing unit, wherein the SN reading unit and the SN writing unit adopt contact buttons.
Fig. 3 is a flowchart illustrating a method for detecting an electric femto according to an exemplary embodiment, and referring to fig. 3, the method is applied to any one of the above-mentioned detection systems, and the method includes the following steps.
Step S11, responding to a first confirmation operation of a user, and generating a first side control signal of the electric flight reach;
step S12, controlling the electric flight path to perform first side operation according to the first side control signal;
and S13, if the first side corresponding to the electric flight is not operated, generating a fault signal to perform fault early warning.
It can be understood that, in the embodiment of the present disclosure, the electric aircraft is caused to respond correspondingly according to the control instruction by a relevant control instruction clicked by a user in the above-mentioned inspection system, and when the response action of the electric aircraft is inconsistent with the control instruction, it is determined that the electric aircraft sends a fault.
Further, the method further comprises:
generating a reset signal of the electric flight in response to a second confirmation operation by a user;
and resetting the electric feeder according to the reset signal.
In an example, an embodiment of the present disclosure further provides an action flow of the electric flight reach, where the specific action flow is as follows:
1. connecting a 24V power supply and an electric flight communication line, pressing down a main power switch of the instrument, lighting up a screen of the instrument at the moment, and displaying related self-construction information and a main picture;
2. pressing the femto power light touch key of the instrument panel, and turning off the femto power of the screen into femto power on;
3. pressing a reset key of a panel to touch a key lightly, sending a reset instruction to the femto by the instrument, completing reset after the femto receives the instruction, giving the control right of the femto to the instrument, and simultaneously displaying the serial number and the version number of the current femto on a screen;
4. pressing a left start key or a right start key of the panel to test the situation that a feeding motor of the flight is not operated;
5. and determining that the femto power button is pressed again when the femto action is abnormal, and closing the femto power to finish the test.
It should be noted that, in the testing process, pressing the left start or right start more than 10 times will enter the automatic continuous testing mode, and if the test is to be stopped, only the stop key needs to be pressed.
Further, the method further comprises:
acquiring an SN number of the electric Feida;
and controlling the electric flight arrival to enter a test mode according to the SN number.
For example, an embodiment of the present disclosure further provides a method for changing an electric femto serial number, where for the femto that has changed the femto control card, the mode needs to be executed, and a corresponding action flow is as follows:
1. connecting a 24V power supply and a flight communication line;
2. pressing a metal switch of a main power supply of the instrument, and lightening a screen of the instrument at the moment and displaying related information and a main picture;
3. pressing SN reading button, activating bar code reading sensor, aligning bar code reader to bar code on the boomerang, reading SN number of the boomerang (if scanned SN data format not of standard boomerang, screen will display serial number illegal);
4. pressing SN write-in key, the instrument will turn on the femto power supply to send femto reset instruction, femto reset, the instrument acquires the control right of femto, then sends data write-in instruction, then writes femto serial number, then turns off the power supply, then turns on the power supply, resets femto again, reads the newly written serial number, and compares with the serial number scanned and input, if the same, displays that serial number write-in is completed, and enters femto test mode. If not, indicating that the sequence number write failed.
It is worth mentioning that after the SN writing key is pressed, all the processes are automatically completed by the instrument, wherein SN input can also be scanned and input by generating an APP generating screen code through a barcode of a smart phone.
Through above-mentioned scheme, provide a provider's electronic flight and reach detecting system, the system includes: the system comprises a singlechip control module, a flight control module and a flight communication module; the single chip microcomputer control module is connected with the flight control module and the flight communication module; the system comprises a flight control module, a singlechip control module and a communication module, wherein the flight control module is used for generating a flight control signal and sending the flight control signal to the singlechip control module; the single chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module; and the flight communication module is used for sending the flight control instruction to the electric flight so as to enable the electric flight to execute corresponding control operation. Therefore, the control of the electric flight controller is realized through the singlechip control module, and the electric flight controller detects the electric flight controller according to flight controller control signals input by the flight controller. The detection of the electric feeder is integrated in a small single chip microcomputer system, so that the detection of the electric feeder is more convenient, and the detection cost of the electric feeder is reduced.
Based on the same inventive concept, embodiments of the present disclosure also provide an electronic device, and referring to fig. 4, fig. 4 is a block diagram of an electronic device shown according to an exemplary embodiment. The electronic device may be a device capable of data processing independent of the terminal device, and may be carried on the terminal device in the form of hardware or software. The terminal equipment can be an intelligent mobile terminal such as a mobile phone and a tablet personal computer, and can also be a fixed terminal.
In this embodiment, the terminal device to which the electronic device belongs at least includes an output module 110, a processor 120, a memory 130, and a communication module 140.
The memory 130 stores an operating system and a terminal application control program, and the electronic device can store a resource use request on the monitored terminal, approval result information fed back from the approval terminal, and authorization credential information in the memory 130; the output module 110 may be a display screen, a speaker, etc. The communication module 140 may include a WIFI module, a mobile communication module, a bluetooth module, and the like, and communicates with an external device or a server through the communication module 140.
Wherein the resource management program in the memory 130 when executed by the processor implements the steps of:
generating a first side control signal of the electric flight in response to a first confirmation operation of a user;
controlling the electric flight path to perform first side operation according to the first side control signal;
and if the first side corresponding to the electric flight reach does not act, generating a fault signal to perform fault early warning.
Further, the resource manager in memory 130, when executed by the processor, performs the steps of:
generating a reset signal of the electric flight in response to a second confirmation operation by a user;
and resetting the electric feeder according to the reset signal.
Further, the resource management program in the memory 130 when executed by the processor implements the steps of:
acquiring an SN number of the electric Feida;
and controlling the electric flight arrival to enter a test mode according to the SN number.
Through above-mentioned scheme, provide a provider's electronic flight and reach detecting system, the system includes: the system comprises a singlechip control module, a flight control module and a flight communication module; the single chip microcomputer control module is connected with the flight control module and the flight communication module; the system comprises a flight control module, a singlechip control module and a communication module, wherein the flight control module is used for generating a flight control signal and sending the flight control signal to the singlechip control module; the single chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module; and the flight communication module is used for sending the flight control instruction to the electric flight so as to enable the electric flight to execute corresponding control operation. Therefore, the control of the electric flight reach is realized through the single-chip microcomputer control module, and the electric flight reach is detected according to the flight reach control signal input by the flight reach control module. The detection of the electric feeder is integrated in a small single chip microcomputer system, so that the detection of the electric feeder is more convenient, and the detection cost of the electric feeder is reduced.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that various changes and modifications can be made by those skilled in the art without departing from the spirit of the invention, and these changes and modifications are all within the scope of the invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (10)
1. An electric femto-sensing system, the system comprising: the system comprises a singlechip control module, a flight control module and a flight communication module; the single chip microcomputer control module is connected with the flight control module and the flight communication module;
the system comprises a single chip microcomputer control module, an access control module and an access control module, wherein the access control module is used for generating an access control signal and sending the access control signal to the single chip microcomputer control module;
the single-chip microcomputer control module is used for converting the flight control signal into a flight control instruction and sending the flight control instruction to the flight communication module;
the femto-cell communication module is used for sending the femto-cell control command to the electric femto-cell so as to enable the electric femto-cell to execute corresponding control operation.
2. The detection system of claim 1, further comprising: the display module is connected with the single chip microcomputer control module;
the flight communication module can be further used for monitoring the running state information of the electric flight and sending the running state information to the single chip microcomputer control module;
the single chip microcomputer control module can also be used for sending the running state information to the display module;
and the display module is used for displaying the running state information in the corresponding display area.
3. The detection system of claim 2, wherein the powered femto further comprises an identity barcode, the system further comprising: the bar code scanning input module is connected with the single chip microcomputer control module;
the bar code scanning input module is used for scanning the identity bar code corresponding to the electric flight platform, generating an identity serial number according to the identity bar code and sending the identity serial number to the single-chip microcomputer control module;
the single chip microcomputer control module is used for binding the identity serial number with the electric flight access strongly and sending the identity serial number to the display module;
the display module is used for displaying the identity serial number in the display area.
4. The detection system of claim 1, wherein the reach control module comprises: the system comprises a femto power switch unit, a femto reset unit, a first side detection unit, a second side detection unit, an SN reading unit and an SN input unit;
the flight power supply switch unit is used for generating a power supply starting signal and sending the power supply starting signal to the single-chip microcomputer control module;
the flight arrival resetting unit is used for generating a resetting signal and sending the resetting signal to the single-chip microcomputer control module;
the first side detection unit is used for generating a first detection control signal corresponding to a first side position of the electric flight reach and sending the first detection control signal to the single chip microcomputer control module;
the second side detection unit is used for generating a second detection control signal of the electric flight reach corresponding to a second side position and sending the second detection control signal to the single-chip microcomputer control module;
the SN reading unit is used for reading an SN serial number of the electric flight and sending the SN serial number to the single chip microcomputer control module;
the SN input unit is used for inputting a target SN serial number of the electric flight and sending the target SN serial number to the single-chip microcomputer control module.
5. The detection system of claim 1, further comprising: the power input module is connected with the single-chip microcomputer control module;
and the power supply input module is used for inputting electric energy to the singlechip control module.
6. The detection system of claim 1, further comprising: the clock module is connected with the single-chip microcomputer control module;
the clock module is used for generating a clock signal and sending the clock signal to the single chip microcomputer control module.
7. An electric flight detection method applied to the detection system according to any one of claims 1 to 7, comprising:
generating a first side control signal of the electric flight in response to a first confirmation operation of a user;
controlling the electric flight path to perform first side operation according to the first side control signal;
and if the first side corresponding to the electric flight reach does not act, generating a fault signal to perform fault early warning.
8. The detection method according to claim 7, further comprising:
generating a reset signal of the electric flight in response to a second confirmation operation by a user;
and resetting the electric feeder according to the reset signal.
9. The method of detecting according to claim 7, further comprising:
acquiring an SN number of the electric Feida;
and controlling the electric flight arrival to enter a test mode according to the SN number.
10. An electronic device comprising a computer program, characterized in that the computer program, when being executed by a processor, carries out the steps of the method of detection of an electric fly-by according to claims 7-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210928794.2A CN115291547A (en) | 2022-08-03 | 2022-08-03 | Electric flight-reach detection system and method and electronic equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210928794.2A CN115291547A (en) | 2022-08-03 | 2022-08-03 | Electric flight-reach detection system and method and electronic equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115291547A true CN115291547A (en) | 2022-11-04 |
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|---|---|---|---|
| CN202210928794.2A Pending CN115291547A (en) | 2022-08-03 | 2022-08-03 | Electric flight-reach detection system and method and electronic equipment |
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| CN (1) | CN115291547A (en) |
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- 2022-08-03 CN CN202210928794.2A patent/CN115291547A/en active Pending
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