CN113626334A - Method, system, medium, terminal and unmanned aerial vehicle for testing airplane functions - Google Patents
Method, system, medium, terminal and unmanned aerial vehicle for testing airplane functions Download PDFInfo
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- CN113626334A CN113626334A CN202110967284.1A CN202110967284A CN113626334A CN 113626334 A CN113626334 A CN 113626334A CN 202110967284 A CN202110967284 A CN 202110967284A CN 113626334 A CN113626334 A CN 113626334A
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- 238000012360 testing method Methods 0.000 title claims abstract description 53
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- 238000004590 computer program Methods 0.000 claims description 6
- 238000010998 test method Methods 0.000 claims description 5
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- G—PHYSICS
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- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Prevention of errors by analysis, debugging or testing of software
- G06F11/362—Debugging of software
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- G06F8/00—Arrangements for software engineering
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
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Abstract
The invention discloses a method, a system, a medium, a terminal and an unmanned aerial vehicle for testing airplane functions, and relates to the technical field of unmanned aerial vehicles. Modifying the firmware of a specific airplane, and adding a specified rgbw judgment parameter value in a light setting interface; judging that a specified software debugging interface is added in the interface; updating the firmware of the cluster by the modified specific firmware through a ground station updating interface; configuring an rgbw lamp light value and sending the rgbw lamp light value to the airplane; calling and realizing a specific test function interface, and counting data and effects; and upgrading the airplane performance firmware back to the main firmware, and normally using the airplane main firmware. The method for testing the airplane function through the rgbw lamp setting interface calls the specific software program interface by setting different rgbw lamp light values to complete the initial test of the specific firmware software and the calling of the unusual function, thereby solving the technical effect that the ground station operation interface needs to be optimized when a new function is added every time.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a method, a system, a medium, a terminal and an unmanned aerial vehicle for testing airplane functions through a light setting interface.
Background
In the team performance industry, sometimes small functions need to be tested and verified, such as upgrading of a bootstrap program of a microcontroller and other unusual functions, and the significance is small because a key is independently pressed on a ground station aiming at the project; and some initial unstable function tests directly modify the ground station interface and are not suitable.
At present, the new functions of the airplane for formation performance are added, corresponding buttons are required to be added on a ground station interface, or specific airplane firmware is configured to perform interface calling within specified power-on time, the scheme is unreasonable, the former consumes time, and the latter is relatively tight in time card and cannot meet actual use.
Designing a debugging phase and calling some use schemes of the unusual functions become problems to be solved.
Through the above analysis, the problems and defects of the prior art are as follows:
(1) in the prior art, the operation interface of the ground station needs to be optimized every time a new function is added.
(2) In the prior art, the time consumption of adding new functions when the formation performance airplane is used is high, and the actual using effect is poor.
The significance of solving the problems and the defects is as follows: the invention solves the software design barrier in the debugging stage and in the use of some unusual functions, and reduces the development time cost and the debugging time cost.
Disclosure of Invention
In order to overcome the problems in the related art, the disclosed embodiments of the present invention provide a method, system, medium, and terminal for testing an airplane function through a light setting interface. In particular to a method for testing airplane functions through an rgbw lamplight setting interface, which comprises the following steps:
according to a first aspect of the disclosed embodiments of the present invention, there is provided a method for testing aircraft functions through a light setting interface, comprising:
the light setting buttons are configured through the ground station, different rgb light values are configured, and the calling of the light interface function is completed by matching with a software program of the light setting interface in the test firmware, and the function test of the light interface is realized.
In an embodiment of the invention, the performance of the normal firmware runs normally in the calling of the light interface function and the function test of the light interface.
In an embodiment of the present invention, the method for testing the airplane function through the light setting interface further includes:
modifying specific airplane firmware, and adding a specified rgbw judgment parameter value in a light setting interface;
step two, judging that a specified software debugging interface is added in the interface;
step three, updating the firmware of the cluster by the modified specific firmware through a ground station updating interface;
step four, configuring an rgbw lamp light value and sending the rgbw lamp light value to the airplane;
step five, calling and realizing a specific test function interface, and counting data and effects;
and step six, upgrading the airplane performance firmware back to the trunk firmware, and enabling the airplane trunk firmware to be normally used.
In an embodiment of the present invention, the first step is performed before adding the specified rgbw judgment parameter value in the lighting setting interface: the specific firmware light setting interface rgbw value is judged.
In an embodiment of the present invention, the software debugging interface specified in the second step is used for implementing a specific firmware testing function.
In an embodiment of the invention, in said step four configuring the rgbw lamp light values, the rgbw lamp light values are configured by ground station specific rgbw lamp light control.
According to a second aspect of the disclosed embodiments of the present invention, there is provided a system for testing aircraft functions via a light setting interface, comprising:
the ground station is used for modifying the firmware of a specific airplane, adding a specified rgbw judgment parameter value in the light setting interface and sending the parameter value to the airplane;
the judgment interface is used for judging the rgbw value of the specific firmware lamplight setting interface;
the software debugging interface is added in the judging interface and used for realizing the test function of the specific firmware;
the ground station upgrading interface is used for upgrading the firmware of the cluster by the modified specific firmware;
the specific test function interface is used for realizing a specific test function and counting data and effects;
and the performance firmware upgrading module is used for upgrading the performance firmware back to the main firmware.
According to a third aspect of the disclosed embodiments of the present invention, there is provided a program storage medium for receiving user input, the stored computer program causing an electronic device to perform the method for testing aircraft functionality via a light setting interface.
According to a fourth aspect of the disclosed embodiments of the present invention, there is provided an information data processing terminal, which is mounted on an airplane, and includes a memory and a processor, the memory storing a computer program, and the computer program, when executed by the processor, causes the processor to execute the method of testing airplane functions through a light setting interface.
According to a fifth aspect of the disclosed embodiments of the present invention, there is provided an unmanned aerial vehicle, wherein the unmanned aerial vehicle executes the method for testing the function of the aircraft through the light setting interface.
The technical scheme provided by the embodiment of the invention has the following beneficial effects:
the method for testing the airplane function through the rgbw lamp setting interface calls the specific software program interface by setting different rgbw lamp light values to complete the initial test of the specific firmware software and the calling of the unusual function, thereby solving the technical effect that the ground station operation interface needs to be optimized when a new function is added every time.
Compared with the prior art, the invention has the advantages that:
the invention realizes the calling of the function interface of the corresponding test firmware by using the lamplight interface and configuring the specific rgbw parameter value, realizes the quick interface test verification, can cancel the function after the function is completed, and does not influence the main function.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention as disclosed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the present disclosure and together with the description, serve to explain the principles of the disclosure.
Fig. 1 is a flowchart of a method for testing an airplane function through a light setting interface according to an embodiment of the present invention.
Fig. 2 is a schematic diagram of a system for testing an aircraft function through a light setting interface according to an embodiment of the present invention.
In the figure: 1. a ground station; 2. judging an interface; 3. a software debugging interface; 4. a ground station upgrade interface; 5. a specific test function interface; 6. and a performance firmware upgrading module.
Fig. 3 is an interface diagram for recording a boot upgrade log of an airplane when the airplane receives a light parameter set by a ground station according to an embodiment of the present invention.
Detailed Description
Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, like numbers in different drawings represent the same or similar elements unless otherwise indicated. The implementations described in the exemplary embodiments below are not intended to represent all implementations consistent with the present disclosure. Rather, they are merely examples of apparatus and methods consistent with certain aspects of the present disclosure, as detailed in the appended claims.
According to the invention, the special rgbw value is configured through the ground station 1 light setting button, and the special treatment of the light interface in the test firmware is matched to complete the calling of the interface function, so that the rapid function test can be realized, and the performance use of the normal firmware is not influenced.
As shown in fig. 1, the method for testing the airplane function through the rgbw light setting interface according to the embodiment of the disclosure includes:
modifying the firmware of a specific airplane, and adding a specified rgbw judgment parameter value in a light setting interface;
judging that a specified software debugging interface 3 is added in the interface 2;
updating the firmware of the cluster by the modified specific firmware through the ground station updating interface 4;
configuring an rgbw lamp light value and sending the rgbw lamp light value to the airplane;
calling and realizing, counting data and effect of the specific test function interface 5;
and upgrading the airplane firmware back to the main firmware, and normally using the airplane main firmware.
In a preferred embodiment of the present invention, before adding the specified rgbw judgment parameter value to the lighting setting interface, the following steps are performed: the specific firmware light setting interface rgbw value is judged.
In a preferred embodiment of the present invention, the designated software debug interface 3 is used to implement specific firmware test functions.
In a preferred embodiment of the invention, the configuration of the rgbw light values is performed by a ground station 1-specific rgbw light control configuration rgbw light values.
As shown in fig. 2, the present invention provides a system for testing aircraft functions through a light setting interface, comprising:
the ground station 1 is used for modifying the firmware of a specific airplane, adding a specified rgbw judgment parameter value in the light setting interface and sending the parameter value to the airplane;
the judgment interface 2 is used for judging the value of the specific firmware lamplight setting interface rgbw;
the software debugging interface 3 is added in the judging interface 2 and is used for realizing the test function of the specific firmware;
the ground station upgrading interface 4 is used for upgrading the firmware of the cluster by the modified specific firmware;
the specific test function interface 5 is used for realizing a specific test function and counting data and effects;
and the performance firmware upgrading module 6 is used for upgrading the performance firmware back to the main firmware.
The effects of the present invention will be further described with reference to the experimental results.
As shown in fig. 3, the light parameters are set to r: 100, g: 100, b: 100, w: and starting to perform airplane boot upgrade log recording at 100.
Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure disclosed herein. This application is intended to cover any variations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.
It will be understood that the present disclosure is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure should be limited only by the attached claims.
Claims (10)
1. A method for testing airplane functions through a light setting interface is characterized by comprising the following steps:
the light setting buttons are configured through the ground station, different rgb light values are configured, and the calling of the light interface function is completed by matching with a software program of the light setting interface in the test firmware, and the function test of the light interface is realized.
2. A method of testing aircraft functionality via a light setting interface as claimed in claim 1 wherein the normal firmware performance is operating normally during the invocation of light interface functionality and the testing of light interface functionality.
3. The method of testing aircraft functionality via a light setting interface of claim 1, wherein the method of testing aircraft functionality via a light setting interface further comprises:
modifying specific airplane firmware, and adding a specified rgbw judgment parameter value in a light setting interface;
step two, judging that a specified software debugging interface is added in the interface;
step three, updating the firmware of the cluster by the modified specific firmware through a ground station updating interface;
step four, configuring an rgbw lamp light value and sending the rgbw lamp light value to the airplane;
step five, calling and realizing a specific test function interface, and counting data and effects;
and step six, upgrading the airplane performance firmware back to the trunk firmware, and enabling the airplane trunk firmware to be normally used.
4. A method for testing aircraft functionality via a light-setting interface as claimed in claim 3, wherein step one is performed before adding the specified rgbw determination parameter value in the light-setting interface: the specific firmware light setting interface rgbw value is judged.
5. The method for testing airplane functions through the light setting interface as claimed in claim 3, wherein the software debugging interface specified in the second step is used for realizing specific firmware testing functions.
6. Method for testing aircraft functions through a light setting interface according to claim 3, characterized in that in the step four configuring the rgbw light values, the rgbw light values are configured by ground station specific rgbw light control.
7. A system for testing aircraft functions via a light setting interface, implementing a method for testing aircraft functions via a light setting interface as claimed in any one of claims 1 to 6, comprising:
the ground station is used for modifying the firmware of a specific airplane, adding a specified rgbw judgment parameter value in the light setting interface and sending the parameter value to the airplane;
the judgment interface is used for judging the rgbw value of the specific firmware lamplight setting interface;
the software debugging interface is added in the judging interface and used for realizing the test function of the specific firmware;
the ground station upgrading interface is used for upgrading the firmware of the cluster by the modified specific firmware;
the specific test function interface is used for realizing a specific test function and counting data and effects;
and the performance firmware upgrading module is used for upgrading the performance firmware back to the main firmware.
8. A program storage medium for receiving user input, the stored computer program causing an electronic device to perform the method of testing aircraft function via a light setting interface of any of claims 1 to 6.
9. An information data processing terminal, which is mounted on an airplane and comprises a memory and a processor, wherein the memory stores a computer program, and the computer program is executed by the processor, so that the processor executes the method for testing airplane functions through a light setting interface according to any one of claims 1 to 6.
10. An unmanned aerial vehicle, characterized in that the unmanned aerial vehicle executes the method for testing aircraft functions through a light setting interface as claimed in any one of claims 1 to 6.
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| CN202110967284.1A CN113626334B (en) | 2021-08-23 | 2021-08-23 | Method, system, medium, terminal and drone for testing aircraft functions |
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| CN202110967284.1A CN113626334B (en) | 2021-08-23 | 2021-08-23 | Method, system, medium, terminal and drone for testing aircraft functions |
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Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105222807A (en) * | 2015-10-14 | 2016-01-06 | 中国民航大学 | A kind of rotor wing unmanned aerial vehicle precision approach path indicator check system and method for calibration |
| DE102015010918A1 (en) * | 2015-08-20 | 2017-02-23 | Diehl Aerospace Gmbh | Lighting device and light arrangement |
| US9940432B1 (en) * | 2014-11-18 | 2018-04-10 | Amazon Technologies, Inc. | Development of an unmanned aerial vehicle |
| CN208111038U (en) * | 2018-03-15 | 2018-11-16 | 深圳鹰之航航空科技有限公司 | A kind of aircraft screen display integrated test system |
| CN109062790A (en) * | 2018-07-19 | 2018-12-21 | 北京首汽智行科技有限公司 | The upgrading test method of car-mounted terminal bluetooth firmware |
| CN110687921A (en) * | 2019-10-30 | 2020-01-14 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle flight control method and device, electronic equipment and storage medium |
| CN111988891A (en) * | 2020-08-17 | 2020-11-24 | 一飞(海南)科技有限公司 | Unmanned aerial vehicle formation music synchronous light control method and control system and unmanned aerial vehicle |
| CN112449460A (en) * | 2020-11-11 | 2021-03-05 | 一飞(海南)科技有限公司 | RGBW four-color LED light calibration method |
| KR102235407B1 (en) * | 2020-02-07 | 2021-04-02 | 한국기술교육대학교 산학협력단 | Implementation of ar-based drone light show |
| CN113110585A (en) * | 2021-04-28 | 2021-07-13 | 一飞(海南)科技有限公司 | Method and system for flying formation dance step state switching, unmanned aerial vehicle and application |
| CN113282104A (en) * | 2021-06-03 | 2021-08-20 | 一飞(海南)科技有限公司 | Method for airplane GPS data abnormity detection and abnormity confirmation aiming at formation performance |
-
2021
- 2021-08-23 CN CN202110967284.1A patent/CN113626334B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9940432B1 (en) * | 2014-11-18 | 2018-04-10 | Amazon Technologies, Inc. | Development of an unmanned aerial vehicle |
| DE102015010918A1 (en) * | 2015-08-20 | 2017-02-23 | Diehl Aerospace Gmbh | Lighting device and light arrangement |
| CN105222807A (en) * | 2015-10-14 | 2016-01-06 | 中国民航大学 | A kind of rotor wing unmanned aerial vehicle precision approach path indicator check system and method for calibration |
| CN208111038U (en) * | 2018-03-15 | 2018-11-16 | 深圳鹰之航航空科技有限公司 | A kind of aircraft screen display integrated test system |
| CN109062790A (en) * | 2018-07-19 | 2018-12-21 | 北京首汽智行科技有限公司 | The upgrading test method of car-mounted terminal bluetooth firmware |
| CN110687921A (en) * | 2019-10-30 | 2020-01-14 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle flight control method and device, electronic equipment and storage medium |
| KR102235407B1 (en) * | 2020-02-07 | 2021-04-02 | 한국기술교육대학교 산학협력단 | Implementation of ar-based drone light show |
| CN111988891A (en) * | 2020-08-17 | 2020-11-24 | 一飞(海南)科技有限公司 | Unmanned aerial vehicle formation music synchronous light control method and control system and unmanned aerial vehicle |
| CN112449460A (en) * | 2020-11-11 | 2021-03-05 | 一飞(海南)科技有限公司 | RGBW four-color LED light calibration method |
| CN113110585A (en) * | 2021-04-28 | 2021-07-13 | 一飞(海南)科技有限公司 | Method and system for flying formation dance step state switching, unmanned aerial vehicle and application |
| CN113282104A (en) * | 2021-06-03 | 2021-08-20 | 一飞(海南)科技有限公司 | Method for airplane GPS data abnormity detection and abnormity confirmation aiming at formation performance |
Non-Patent Citations (3)
| Title |
|---|
| HYUNGTAE KIM等: "Optimal Color Lighting for Scanning Images of Flat Panel Display using Simplex Search", JOURNAL OF IMAGING, 12 November 2018 (2018-11-12), pages 1 - 12 * |
| 梁计锋: "固定翼飞机平衡装置的研究与设计", 电子设计工程, 31 July 2021 (2021-07-31), pages 61 - 65 * |
| 许梦华;庞振岳;: "基于Qt的多旋翼电动无人机地面站软件设计与实现", 飞机设计, no. 03, 15 June 2020 (2020-06-15) * |
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