摘要
针对惯性组合系统中的多子导航系统，研究了“测量融合”的技术。文中讨论了测量融合的设计思想和方案，以惯性、全球卫星定位系统（ＧＰＳ）、无线电测距测向系统（ＶＯＲ／ＤＭＥ）、地形辅助导航系统（ＴＡＮ）组合导航系统为例，研究了组合导航系统的融合算法，并进行了蒙特·卡洛法仿真计算。结果表明，系统的设计是合理的，为惯性组合导航系统提出了有实用价值的一种融合算法。
In view of existing situation in the inertial integrated system with multi subnavigation system, the measurement fusion technology applying to the integrated system is researched. The design idea and schemes of the measurement fusion are discussed. Taking INS,GPS,VOR/DME and TAN (terrain aided navigation ) for an example, the fusion algorithm of integrated navigation system is analyzed. With these analyses and Monte carlo method simulation, it comes to the conclusion that the design of the measurement fusion navigation system is successful, and possessed practicable value for the inertial integrated system.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
1997年第4期372-377,共6页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
惯性导航
组合导航
数据融合
测量融合
inertial navigation
integrated navigation
data fusion
measurement fusion
Kalman filtering
