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
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2021-12-17
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Abstract
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...
Examples
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...