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采用格型卡尔曼滤波的航空浮标定位算法研究
引用本文:张欣,杨日杰,赵耀. 采用格型卡尔曼滤波的航空浮标定位算法研究[J]. 测试技术学报, 2005, 19(2): 195-199
作者姓名:张欣  杨日杰  赵耀
作者单位:海军航空工程学院青岛分院,航空电子系,山东,青岛,266041;海军航空工程学院,电子工程系,山东,烟台,264001
摘    要:根据航空搜潜声呐浮标与飞机的相对方位信息,采用格型扩展卡尔曼滤波技术,对航空浮标定位方法进行了研究,建立了状态简化的2-状态定位系统的数学模型;利用蒙特卡洛仿真法,从位置估计的相对误差和均方误差两个方面,仿真分析了系统的误差性能,并获得了较好的效果。

关 键 词:航空反潜  浮标定位  相对方位角  格型卡尔曼滤波器  仿真
文章编号:1670-7449(2005)02-0195-05
收稿时间:2004-09-13
修稿时间:2004-09-13

Research of Buoy Position Calculation Method Which Based on Lattice Extended Kalman Filter
ZHANG Xin,Yang Ri-jie,Zhao Yao. Research of Buoy Position Calculation Method Which Based on Lattice Extended Kalman Filter[J]. Journal of Test and Measurement Techol, 2005, 19(2): 195-199
Authors:ZHANG Xin  Yang Ri-jie  Zhao Yao
Abstract:According to the relative orientation information received between the airplane and aerial anti-submarine buoy, the lattice extended kalman filtering technique is used to research the buoy location method. The mathematical model for the simplification of two-state location system is established. By using Monte-Carlo simulation arithmetic, the relative position errors and RMS error about position estimation and the system uncertainty are simulated and analyzed, Better tesults have been acquired.
Keywords:Aerial anti-submarine   buoy location   relative azimuth angle   lattice kalman filter   aimulation
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