Test platform construction method and test method for unmanned aerial vehicle flight control management software

Abstract

The embodiment of the invention discloses a test platform construction method and test method for unmanned aerial vehicle flight control management software. The method comprises the steps: building an interface of the unmanned aerial vehicle flight control management software, and the interface comprises an internal interface and an external interface of the unmanned aerial vehicle flight controlmanagement software; establishing a virtual target machine for operating the unmanned aerial vehicle flight control management software according to the internal interface; establishing a distributedsimulation data bus, and connecting the unmanned aerial vehicle flight control management software and the external simulation subsystem through the distributed simulation data bus; and establishingan external simulation subsystem for simulating the external environment subsystem according to the external interface. According to the embodiment of the invention, by establishing a peripheral equipment digital simulation environment associated with unmanned aerial vehicle flight control and management system software and integrating mature test analysis and management tools, a comprehensive test method for white box test, black box test and static analysis of the unmanned aerial vehicle flight control and management system software is carried out on the basis of the peripheral equipment digital simulation environment.

Description

technical field [0001] This application relates to, but is not limited to, the field of airborne electronic technology, especially a test platform construction method and test method for UAV flight control management software. Background technique [0002] Integrated avionics and fire control system software and hardware integrated design technology has been widely used in various types of modern military aircraft. UAV flight control and management system software realizes the core functions of aircraft flight and combat missions. At present, in the research and development mode of UAV flight control and management system software, most of the system design is carried out first, and then the hardware equipment reaches the delivery status. Integration testing and validation such as figure 1 As shown, it is a schematic diagram of the system configuration of the UAV flight control management software in the embodiment of the present invention, which contains the flight control...

AI Technical Summary

Problems solved by technology

[0009] f) Or, it often occurs that the only set of real hardware environment is developing and testing a certain version of UAV flight control and management system software functions, and it is impossible to test another version of UAV flight control and management system software at the same time , Delayed the test plan and software product installation plan

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