摘要
研究了机载无源定位系统的仿真环境建立,提出了仿真各种飞行姿态和飞行轨迹时如何确定信息量及其误差分布。由于信息量分布于不同的坐标系中,最后推导出了三个坐标系之间的转换矩阵。经某工程项目应用,取得了较好效果。
How to establish a simulation for airborne passive direction system is investigated in this paper. How to ascertain information estimates and errors when simulating aviation carriage and track are posed. At last, transform matrix between three coordinates is deduced. Applying these results to an engineering project shows good impression.
出处
《计算机仿真》
CSCD
2003年第9期27-28,134,共3页
Computer Simulation
