A multi-bus interface system of an airborne transponder
An interface system and multi-bus technology, which is applied in the field of airborne transponder multi-bus interface system, can solve the problems of increased waiting time for repeated design, complex types and models of airborne transponders, increased repeated design costs and management costs, etc., to reduce The effect of scientific research cost and manpower management cost, reduction of repeated production, and risk reduction
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[0030] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.
[0031] Any feature disclosed in this specification, unless specifically stated, can be replaced by other alternative features that are equivalent or have similar purposes. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.
[0032] figure 1 The structural block diagram of the multi-bus interface system provided for the embodiment of the present invention, such as figure 1 As shown, it includes a multi-bus input module, a logic control module, a data processing module and an output module, the logic control module includes a protocol analysis module and a parallel bus logic control module, and the multi-bus input module passes through the protocol analysis module or directly It is correspondingly connected with the paral...
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