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基于低成本传感器的航弹组合导航算法
引用本文:翟萌.基于低成本传感器的航弹组合导航算法[J].兵工自动化,2016,35(4):16-20.
作者姓名:翟萌
作者单位:南京理工大学智能弹药国防重点实验室,南京,210094
摘    要:为了降低航弹成本、提升装备效费比,以低成本航空制导炸弹的组合导航系统为研究对象进行算法研究.利用扩展卡尔曼滤波算法构建以MEMS陀螺和加速计为核心,GPS辅助的低成本、高精度组合导航系统,采用无人机飞行试验对该系统的导航性能进行评估,得出误差数据,并与纯惯性导航结果相对比.实验结果表明:该导航系统定位精度能达到2 m以内,系统解算精度满足航空制导炸弹飞行要求,对常规航弹制导化改造具有工程实际意义.

关 键 词:航空制导炸弹  惯性导航  GPS/INS组合导航  扩展卡尔曼滤波
收稿时间:2015/8/31 0:00:00
修稿时间:2015/9/24 0:00:00

Aviation Bomb Integrated Navigation Algorithm Used on Low-cost Sensor
Zhai Meng.Aviation Bomb Integrated Navigation Algorithm Used on Low-cost Sensor[J].Ordnance Industry Automation,2016,35(4):16-20.
Authors:Zhai Meng
Affiliation:Zhai Meng;Jia Fangxiu;Yu Jiyan;National Key Laboratory of Smart Ammunition, Nanjing University of Science & Technology;
Abstract:To reduce the cost of bomb and enhance the equipment efficiency cost ratio, an algorithm research about integrated navigation system for low cost guided aviation bomb. A low cost and high precision combined navigation system is then developed by using extended Kalman filter algorithm, MEMS gyroscope and accelerometer assisted by GPS. UAV flight experimental data is carried out to verify the navigation system, and get the error data. The results are subsequently compared to the stand-alone inertial navigation solution. The experiment results show that the positioning accuracy of this system can reach 2 meters, which can satisfy the requirement of guided aviation bomb flight. In addition, it has engineering practical significance for updating regular conventional bomb.
Keywords:guided aviation bomb  inertial navigation  GPS/INS integrated navigation system  extended Kalman filter
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