Design and Implementation of the Tightly-coupled SINS / GPS Integrated Navigation System Based on FPGA for Target Missile
A novel architecture of tightly-coupled SINS/GPS integrated navigation system based on FPGA for target missile is proposed in this paper.The whole system is built on a single single FPGA chip containing a Nios Ⅱ soft-core processor.In addition,the embedded real-time operating system μC/OS-Ⅱ is transplanted to the Nios Ⅱ processor for managing each module in the system.The system can still provide the high-precision navigation data to integrated control computer of target missile when the number of available satellites is less than 4 by means of processing the pseudorange and pseudorange rate seprately.Therefore,the system has the strong application significance in terms of reducing the route shortcut of target missile.
tightly-coupled GPS SINS FPGA μC/OS-Ⅱ
Guo Jingjie Cai Xiaofeng He Chao
91851 Unit,Huludao,Liaoning Province,P.R.China
国际会议
济南
英文
287-290
2012-12-29(万方平台首次上网日期,不代表论文的发表时间)