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基于多传感器信息融合理论的无人机相对导航状态估计方法
引用本文:金红新,杨涛,王小刚,周国峰,姚旺.基于多传感器信息融合理论的无人机相对导航状态估计方法[J].国防科技大学学报,2017,39(5).
作者姓名:金红新  杨涛  王小刚  周国峰  姚旺
作者单位:国防科学技术大学 航天科学与工程学院,国防科学技术大学 航天科学与工程学院,哈尔滨工业大学,中国运载火箭技术研究院,中国运载火箭技术研究院
摘    要:为提升无人机的作战效能和作战指标,提升无人机的相对导航精度和导航系统可靠性,本文以无人机编队的相对导航系统为研究背景,基于容积卡尔曼滤波算法和信息滤波算法,研究了容积信息滤波算法。此外,还采用了多传感器信息融合理论,利用分布式信息融合结构构建了无人机相对导航滤波器,对来自惯导、视觉和卫星的信息进行融合,获取无人机间的相对位置、速度和姿态信息。该方法提升了无人机相对导航的导航精度、导航可靠性和滤波稳定性,容积信息滤波算法的应用避免了传统滤波算法在在高维系统中出现的数值不稳定以及精度降低等问题。论文还进行了相应的数学仿真,仿真结果表明该方法提高了无人机编队之间相对导航的精度和可靠性,证明了算法的有效性。

关 键 词:无人机  多传感器信息融合  相对导航
收稿时间:2017/6/20 0:00:00
修稿时间:2017/6/21 0:00:00

UAV Relative Navigation Method Research Based on Multi-sensor Information Fusion
Abstract:In order to improve the operational effectiveness and operational indicators of the unmanned aerial vehicle (UAV), enhance the accuracy and reliability of the UAV relative navigation system, a novel relative navigation method is proposed in this paper. Under the background of relative navigation system, the cubature information filter is researched based on the cubature Kalman filter and information filter. Moreover, an INS/GPS/VisNav relative navigation filter is designed by making use of the multi-sensor information fusion theory and distributed information fusion structure to fuse the information from INS, VisNav and GPS, and then the relative position, velocity and attitude are obtained. By making use of this algorithm, the accuracy, reliability and stability of the reliability navigation system are all improved. In addition, the accuracy decrease and numerical instability which often occur to traditional filter is avoided by cubature information filter. Some simulations are conducted in this paper. The simulation results indicate the method could improve the accuracy and reliability of the UAV relative navigation system, and the algorithm proposed in the paper is verified.
Keywords:UAV  Multi-sensor Information Fusion  Relative Navigation
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