Design of Hardware-in-the-loop Simulation System to UAV Landing Guidance
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.
无人飞机 自动着舰导引 硬件仿真 数值模拟
Hu Yiming Qin Yongyuan Wu Dewei
College of Automation of Northwestern Polytechnical University,Xi”an,710072,china The Telecommunication Engineering Institute of Air Force Engineering University
国内会议
南京
英文
145-149
2008-02-01（万方平台首次上网日期，不代表论文的发表时间）