Design of Hardware-in-the-loop Simulation System to UAV Landing Guidance

摘要

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．