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空投系统航向测量方法研究
引用本文:王锐.空投系统航向测量方法研究[J].科学技术与工程,2012,12(4):843-847.
作者姓名:王锐
作者单位:西北工业大学自动化学院,西安,710072
摘    要:航向信息是空投系统运行中一个非常重要的参数,磁航姿系统能够利用地磁场来测量载体的姿态信息,体积小、精度高,但却易受外界磁场的干扰,而惯性器件恰好具有不受环境磁场影响的特性,我们可以将两种传感器组合起来,共同测量载体的航向信息。经过仿真验证,外部姿态信息的引入极大改善了系统的航向误差,满足空投系统应用需求。

关 键 词:航向测量  卡尔曼滤波  磁罗盘    MEMS陀螺
收稿时间:2011/11/15 0:00:00
修稿时间:2011/11/30 0:00:00

The Research Of Heading Measure Method For Airdrop System
wangrui.The Research Of Heading Measure Method For Airdrop System[J].Science Technology and Engineering,2012,12(4):843-847.
Authors:wangrui
Institution:(School of Automation NWPU,Xi’an 710072,P.R.China)
Abstract:Heading information is a very important parameter during the precision airdrop system. Magnetic attitude system uses geomagnetic field to measure the attitude information of the vehicle. It has some merits such as small size, high precision and stable performance. However, it also has the inherent characteristic of sensitive to the external interferences, while the Rate gyroscope of inertial device does not have such shortcoming. Thus we can combine the two types of these sensors to measures the heading information. Simulation results prove that the heading error can be improved greatly as the introduction of external attitude information, which meets the precision airdrop system.
Keywords:Heading measure  Kalman filter  Magnetic compass  Gyroscope of MEMS
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