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the UAV ILS is key component to realization of UAV automatic landing.How to design and test the stability,reliability and performance indicators of landing guidance system，and not spend a lot of financial and material resources for the actual flight risL become an important topic in the project development.This paper describes the design of a Hardware-in-the-loop Simulation system that can practical alternative to flight tests，and the maximum simulated instrument landing system to guide UAV landing.