摘要
为保证飞行器的导航精度及可靠性 ,采用了惯导 /GNSS/罗兰 C/航姿系统的组合导航。该组合导航采用开环组合方式 ,将多系统导航信息在计算机中进行综合 ,提高导航信息精度。仿真试验结果说明 ,所设计的组合导航系统是可行的 。
The integraed navigation system of inertial navigation system(INS),GNSS,LoranC,and HARS are used to ensure the aerocraft navigation precision and reliability.The integrated system adopts an integrated mode of openloop which combines navigation information of many systems in computer to improve navigation precision.The test result shows that the integrated navigation system is feasible,and meets the requirments of the task.
出处
《中国惯性技术学报》
EI
CSCD
2000年第3期12-16,共5页
Journal of Chinese Inertial Technology
