Formation aircraft control component upgrading method and system, medium, formation aircraft and application

A technology of aircraft control and components, applied in the direction of control/adjustment system, non-electric variable control, three-dimensional position/course control, etc., to solve the problem of upgrading and improve the effect of flexibility

Pending Publication Date: 2021-12-17
一飞智控(天津)科技有限公司
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Problems solved by technology

[0003] Through the above analysis, the existing problems and defects of the existing technology are: the writing of the hardware version information of individual aircraft through the writing in the production stage, and the mixing of different batches and different hardware versions by relying on the hardware version information when the aircraft components are upgraded in the subsequent stage. Together the aircraft to achieve overall compatible upgrade

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  • Formation aircraft control component upgrading method and system, medium, formation aircraft and application
  • Formation aircraft control component upgrading method and system, medium, formation aircraft and application

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Embodiment

[0058] The methods for supporting the upgrade of multi-hardware version formation aircraft control components specifically include:

[0059] Step 1, during aircraft production, input aircraft component hardware information into OTP module 1.

[0060] Step 2, receive the upgrade command, check and confirm the component hardware, and obtain the current firmware version of the formation aircraft component;

[0061] Step 3, perform hardware version query to obtain component hardware version;

[0062] Step 4, access the hardware OTP, and read the OTP information;

[0063] Step 5, upgrade different versions of firmware for aircraft with different types of hardware versions.

[0064] In a preferred embodiment of the present invention, the information read in step 4 includes:

[0065] For aircraft with hardware version information V1.0.2, the hardware version of component A used is V1;

[0066] The hardware version of component B is V3...;

[0067] Hardware version information Th...

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Abstract

The invention belongs to the technical field of unmanned, and discloses a formation aircraft control component upgrading method and system, a medium, a formation aircraft and application. The method comprises: receiving an upgrading instruction, performing component hardware query confirmation, and obtaining a current firmware version of the formation aircraft component; carrying out hardware version query to obtain a component hardware version; accessing a hardware OTP (One Time Programmable), and reading OTP information; and upgrading different versions of firmware for aircrafts with different types of hardware versions. According to the design method for supporting upgrading of the multi-hardware version formation aircraft control component, the aircraft component is identified firstly, then hardware version information of a known component type is accessed, different types of firmware are selected and upgraded according to different hardware versions of different components, and simultaneous upgrading of the formation fleet aircrafts with multiple versions and multiple types of hardware is realized. The problem of upgrading after mixing of aircrafts with different hardware is solved.

Description

technical field [0001] The invention belongs to the field of unmanned technology, and in particular relates to a method and system for upgrading control components of formation aircraft supporting multiple hardware versions, a terminal for upgrading control components of formation aircraft, a computer-readable storage medium, formation aircraft, and an application. Background technique [0002] At present, in the flight demonstration process of formation aircraft, there is a problem that different batches of aircraft have different hardware versions. Troublesome problems of distinguishing and categorizing landing planes. Designing a method for upgrading targeted firmware for different hardware version types has become a problem to be solved. [0003] Through the above analysis, the existing problems and defects of the existing technology are: the writing of the hardware version information of individual aircraft through the writing in the production stage, and the mixing of...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F8/65G05D1/10
CPCG06F8/65G05D1/104
Inventor 张沐然赵晓伟
Owner 一飞智控(天津)科技有限公司
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