Abstract
According to the analysis on the composition as well as functions of flight control system of unmanned aerial vehicle (UAV), the computer simulation test method of flight control and management based on simulation test platform is introduced, with the focus on fault injection and test method. Thereby putting forward the construction principle and test method for simulation test environment of flight control system. In the end, the follow-up development of the dynamic simulation test of UAV flight control system is pointed out.
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