CN113848852B - Method, system, terminal, medium and application for forming firmware version return of airplane - Google Patents

Method, system, terminal, medium and application for forming firmware version return of airplane Download PDF

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Publication number
CN113848852B
CN113848852B CN202111135488.5A CN202111135488A CN113848852B CN 113848852 B CN113848852 B CN 113848852B CN 202111135488 A CN202111135488 A CN 202111135488A CN 113848852 B CN113848852 B CN 113848852B
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aircraft
firmware version
ground station
version information
linux
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CN113848852A (en
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张沐然
赵晓伟
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Efy Intelligent Control Tianjin Tech Co ltd
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Efy Intelligent Control Tianjin Tech Co ltd
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • G05B23/0205Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0208Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system
    • G05B23/0213Modular or universal configuration of the monitoring system, e.g. monitoring system having modules that may be combined to build monitoring program; monitoring system that can be applied to legacy systems; adaptable monitoring system; using different communication protocols
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/20Pc systems
    • G05B2219/24Pc safety
    • G05B2219/24065Real time diagnostics

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and discloses a method, a system, a terminal, a medium and an application for firmware version return of a formation aircraft. The Arm-linux onboard APP acquires firmware version information of each part of the aircraft component and sorts the firmware version information into big package data; the communication board application component reports the sorted big packet data to the ground station; and the ground station transmits the reported instruction back to the Arm-linux on-board APP, inquires and displays the big packet data. According to the design method for the firmware version feedback of the formation aircraft, provided by the invention, the detailed version information display function of the formation aircraft is realized by counting the version information of each part of the aircraft and then packaging the version information into the feedback ground station and uniformly displaying the version information on the ground station interface, so that the time consumption caused by checking the version of the aircraft is reduced.

Description

Method, system, terminal, medium and application for forming firmware version return of airplane
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a method, a system, a terminal, a medium and an application for firmware version return of a formation aircraft.
Background
At present, in the field of the industry of the flight performances of the formation aircraft, the problem of flight abnormality caused by non-uniform version information of individual aircraft groups exists, so that firmware versions of all parts of the aircraft need to be checked separately for each flight performance before each flight performance, and then the flight performance is carried out, thereby leading to complex and complicated overall operation flow, time consumption and labor consumption. Designing a scheme for forming firmware version backhaul of an aircraft becomes a problem to be solved.
Through the above analysis, the problems and defects existing in the prior art are as follows:
(1) The formation fleet aircraft is difficult to unify aircraft versions, the aircraft comprises components of all parts, the pendant version of the components is unknown, under the condition that the firmware version is unknown, independent inspection is needed, time and labor are consumed, omission occurs, and aeroperformance accidents can be caused.
(2) In the prior art, because individual version information of the fleet aircraft is not uniform, performance effects are easily deteriorated when aeroperformance is performed.
The meaning of solving the problems and the defects is as follows: the individual versions of the aircraft group are reported, so that the ground station background unified supervision and upgrading processing are facilitated, the consistency of the aircraft software versions in the formation performance process each time is ensured, and the effect of influencing the performance due to flight errors caused by the abnormality of the software versions is reduced.
Disclosure of Invention
In order to overcome the problems in the related art, the disclosed embodiments of the present invention provide a method, a system, a terminal, a medium and an application for forming firmware version backhaul of an aircraft.
The technical scheme is as follows: a method of forming a firmware version return for an aircraft, comprising:
and counting version information of each part of the aircraft, then packaging and returning the aircraft to the ground station, and uniformly displaying detailed version information of the formation aircraft on a ground station interface.
In an embodiment of the present invention, the method for forming firmware version feedback of an aircraft specifically includes:
firstly, acquiring firmware version information of each part of components of an aircraft by an Arm-linux onboard APP, and arranging the firmware version information into big package data; wherein, arrange big package: combining the software version information of the aircraft component into a data packet in a fixed format and a character string array mode, and then transmitting the data packet to a ground station through a communication link;
step two, the communication board application component reports the sorted big packet data to the ground station;
and step three, the ground station returns the reported instruction in the step two to the Arm-linux on-board APP, inquires and displays the large packet data.
In an embodiment of the present invention, the big packet data consolidated in the step one includes: the information of the flight control Bootloader, the flight control APP, the Arm-linux on-board file system, the Arm-linux on-board equipment tree, the Arm-linux on-board kernel, the application, the u-boot version and the radio station firmware version.
In an embodiment of the present invention, the reporting method in the second step includes:
and after power-on, reporting the ground station by automatically reporting version information and sending an instruction query method by the ground station.
Another object of the present invention is to provide a system for firmware version backhaul of a formation aircraft, comprising:
the Arm-linux on-board APP is used for acquiring firmware version information of each part of the aircraft component and finishing the firmware version information into big package data;
the communication board application component is used for reporting the sorted big packet data to the ground station;
and the ground station is used for returning the reported instruction to the Arm-linux on-board APP, inquiring and displaying the big packet data.
Another object of the present invention is to provide an information data processing terminal, which includes a memory and a processor, where the memory stores a computer program, and the computer program when executed by the processor causes the processor to execute the method for returning the firmware version of the formation aircraft.
Another object of the present invention is to provide a computer readable storage medium storing a computer program which, when executed by a processor, causes the processor to perform the steps of:
and counting version information of each part of the aircraft, then packaging and returning the aircraft to the ground station, and uniformly displaying detailed version information of the formation aircraft on a ground station interface.
It is another object of the present invention to provide a performance forming aircraft that performs the method of forming aircraft firmware version backhauls.
It is another object of the present invention to provide an application of the method for firmware version backhaul of a formed aircraft in a commercial tandem unmanned aircraft formation.
The invention further aims to provide an application of the method for returning the firmware version of the formation aircraft to the formation of the traffic and public security inspection unmanned aerial vehicle.
By combining all the technical schemes, the invention has the advantages and positive effects that:
according to the design method for the firmware version feedback of the formation aircraft, provided by the invention, the detailed version information display function of the formation aircraft is realized by counting the version information of each part of the aircraft and then packaging the version information into the feedback ground station and uniformly displaying the version information on the ground station interface, so that the time consumption caused by checking the version of the aircraft is reduced.
Advantages of the present invention compared to the prior art further include:
by designing statistics of version information of all parts of the aircraft and uniformly returning the version information to the ground station, the information is displayed in an interface, so that time consumption caused by independently checking the version information of individual firmware of the aircraft is greatly solved, and the management time of the firmware version in the operation process is greatly reduced.
In the prior art, the mode of inquiring the independent version information is to connect and communicate the aircraft one by one through a communication interface such as a USB interface or a serial port, and version statistics is carried out, so that the scheme is only used in a development stage in the actual use process, and the time statistics test of batches of aircraft is not carried out.
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 disclosure of the invention as claimed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the disclosure and together with the description, serve to explain the principles of the disclosure.
FIG. 1 is a flow chart of a method for firmware version backtracking of a queued aircraft provided by an embodiment of the present invention.
Fig. 2 is a schematic diagram of a firmware version backhaul system of a formation aircraft according to an embodiment of the present invention.
In the figure: 1. arm-linux on-board APP; 2. a communication board application component; 3. a ground station.
Detailed Description
In order that the above objects, features and advantages of the invention will be readily understood, a more particular description of the invention will be rendered by reference to the appended drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. The invention may be embodied in many other forms than described herein and similarly modified by those skilled in the art without departing from the spirit or scope of the invention, which is therefore not limited to the specific embodiments disclosed below.
It will be understood that when an element is referred to as being "fixed to" 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. The terms "vertical", "horizontal", "left", "right" and the like are used herein for illustrative purposes only and are not meant to be the only embodiments.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. The term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.
The method for transmitting back the firmware version of the formation aircraft provided by the embodiment of the invention comprises the following steps: firstly, acquiring firmware version information of each part of components of an aircraft, and finishing the firmware version information into big package data; the method comprises a flight control Bootloader (start program), a flight control APP, an Arm-linux on-board file system, an Arm-linux on-board equipment tree, an Arm-linux on-board kernel, an application, a u-boot version, a radio station firmware version and the like.
Transmitting the big packet data to the ground station 3 through the communication board application component 2;
there are two reporting methods, namely, the method for reporting version information and the method for inquiring instructions sent by the ground station 3 after the aircraft is powered on.
The ground station 3 transmits a query instruction of the big packet data to an Arm-linux (embedded operating system) on-board APP, and performs query display of the big packet data.
The technical scheme of the invention is further described below with reference to specific embodiments.
Examples
In an embodiment of the present invention, as shown in fig. 1, a method for returning firmware versions of a formation aircraft provided in the embodiment of the present invention includes:
firstly, acquiring firmware version information of each part of components of an aircraft by an Arm-linux (embedded operating system) on-board APP, and arranging the firmware version information into big package data;
step two, the communication board application component 2 reports the sorted big packet data to the ground station 3 through automatic version information reporting and a ground station 3 sending instruction inquiry method;
and step three, the ground station 3 transmits the reported instruction of the step two back to an Arm-linux (embedded operating system) on-board APP for inquiring and displaying big packet data.
In step three of a preferred embodiment of the present invention, the queried information comprises:
information such as a flight control Bootloader (starting program), a flight control APP, an Arm-linux on-board file system, an Arm-linux on-board equipment tree, an Arm-linux on-board kernel, an application, a u-boot version, a radio station firmware version and the like.
As shown in fig. 2, the present invention provides a firmware version backhauling system for a formation aircraft, comprising:
the Arm-linux on-board APP 1 is used for acquiring firmware version information of each part of the aircraft component and finishing the firmware version information into big package data;
the communication board application component 2 is used for reporting the sorted big packet data to the ground station 3;
and the ground station 3 is used for returning the reported instruction to the Arm-linux on-board APP 1, inquiring and displaying the big packet data.
The invention obtains the version information of each component through the aircraft individual, and then transmits the version information back to the ground station 3 together through unified packaging, thereby realizing the detailed display of the integral version information of the cluster and realizing the design scheme of version information statistics and display.
The technical scheme of the invention is further described below with reference to specific application examples.
Application example
By applying the method for returning the firmware version of the formation aircraft provided by the invention, the embedded equipment terminal is used for carrying out the information returning log interface display of the firmware version, and the specific actual test verification flow is shown as follows:
(1) Powering up the aircraft;
(2) An aircraft version information package;
(3) The aircraft version information is uploaded to the ground station 3.
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 adaptations, 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 is to be understood that the present disclosure is not limited to the precise arrangements and instrumentalities shown in the drawings, and that various modifications and changes may be effected without departing from the scope thereof. The scope of the present disclosure should be limited by the attached claims.

Claims (8)

1. A method of forming a firmware version backhaul of an aircraft, the method comprising:
the detailed version information of the formation aircraft is displayed on a ground station interface in a unified way by counting the version information of each part of the aircraft and then packing the information back to the ground station; the method for forming the firmware version return of the airplane specifically comprises the following steps:
firstly, acquiring firmware version information of each part of components of an aircraft by an Arm-linux onboard APP, and arranging the firmware version information into big package data;
step two, the communication board application component reports the tidied big packet data to the ground station;
step three, the ground station returns the reported instruction of the step two to the Arm-linux on-board APP for inquiring and displaying big packet data;
the reporting mode in the second step comprises the following steps:
and after power-on, reporting the ground station by automatically reporting version information and sending an instruction query method by the ground station.
2. The method of claim 1, wherein the step-one consolidated big packet data comprises: the information of the flight control Bootloader, the flight control APP, the Arm-linux on-board file system, the Arm-linux on-board equipment tree, the Arm-linux on-board kernel, the u-boot version and the radio station firmware version.
3. A formation aircraft firmware version backhaul system implementing the method of formation aircraft firmware version backhaul of any one of claims 1-2, the formation aircraft firmware version backhaul system comprising:
the Arm-linux on-board APP is used for acquiring firmware version information of each part of the aircraft component and finishing the firmware version information into big package data;
the communication board application component is used for reporting the tidied big packet data to the ground station;
and the ground station is used for returning the reported instruction to the Arm-linux on-board APP, inquiring and displaying the big packet data.
4. An information data processing terminal, characterized in that it comprises a memory and a processor, said memory storing a computer program which, when executed by said processor, causes said processor to carry out the method of firmware version return of a enqueued aircraft according to any one of claims 1-2.
5. A computer readable storage medium storing a computer program which, when executed by a processor, causes the processor to perform the steps of:
and counting version information of each part of the aircraft, then packaging and returning the aircraft to the ground station, and uniformly displaying detailed version information of the formation aircraft on a ground station interface.
6. A performance formation aircraft, characterized in that it performs a method of firmware version back of the formation aircraft according to any one of claims 1-2.
7. Use of a method of fomiing aircraft firmware version backhauls according to any one of claims 1-2 in a commercial assembly unmanned aircraft fomiing.
8. Use of a method of firmware version backhaul of a formation aircraft as claimed in any one of claims 1 to 2 in transportation, public safety inspection unmanned aerial vehicle formation.
CN202111135488.5A 2021-09-27 2021-09-27 Method, system, terminal, medium and application for forming firmware version return of airplane Active CN113848852B (en)

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Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007310690A (en) * 2006-05-19 2007-11-29 Sharp Corp Update method of firmware, program, storage medium
FR2959633B1 (en) * 2010-04-29 2012-08-31 Airbus Operations Sas METHOD FOR UPGRADING AN AIRCRAFT
CN107357601A (en) * 2016-05-10 2017-11-17 零度智控(北京)智能科技有限公司 Unmanned plane device for upgrading firmware, method and terminal
CN106055373A (en) * 2016-07-04 2016-10-26 苏州光之翼智能科技有限公司 Automatic batch upgrading device and method for unmanned aerial vehicle firmware
CN107797811B (en) * 2016-08-30 2021-05-07 京瓷办公信息系统株式会社 Electronic device, version checking system, and recording medium
WO2018058564A1 (en) * 2016-09-30 2018-04-05 深圳市大疆创新科技有限公司 Upgrade method, upgrade apparatus, upgrade device and upgrade system
CN109254888A (en) * 2018-09-30 2019-01-22 苏州浪潮智能软件有限公司 A kind of method of inspection based on equipment firmware version information
WO2020118639A1 (en) * 2018-12-13 2020-06-18 深圳市大疆软件科技有限公司 Unmanned aerial vehicle and firmware upgrade method thereof
CN111273926A (en) * 2020-01-14 2020-06-12 一飞智控(天津)科技有限公司 Airport client remote upgrade management method, system, storage medium and unmanned aerial vehicle
CN112256508A (en) * 2020-10-23 2021-01-22 广州极飞科技有限公司 Unmanned aerial vehicle self-checking method

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