Automatic identifying and configuring method for airborne multi-redundancy device of general-purpose plane
A technology of automatic identification and configuration method, which is applied to the redundancy of hardware for data error detection, generation of response errors, instruments, etc., can solve problems such as high cost, maintainability, and poor scalability, and achieve Ease of implementation, improved maintainability, and fewer resources
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[0013] The invention adds a built-in U-disk to the airborne cable, and stores system initial configuration scheme files in the U-disk. The system integrated processor defines the cables of all connected devices by reading the configuration scheme file on the U disk, and completes some system initialization work, so that the system can be converted from hardware configuration to software configuration. Moreover, the U disk is built into the installation cable, and the system redundant equipment and system processor can be loaded and unloaded completely independently of the aircraft, thereby improving the maintainability and expandability of the system. Because the use of the storage device of the current USB interface is very mature and reliable, the cost is low.
[0014] First of all, the solution requires a built-in U disk to be solidified on the installation cable, which is only used as the slave disk of the onboard integrated processor, and the interface connection of the U...
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