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模糊自适应滤波方法在相对导航系统中的应用
引用本文:王艳东,韩智华,蔡君亮,陈晓强,吉庆昌. 模糊自适应滤波方法在相对导航系统中的应用[J]. 电光与控制, 2012, 19(10): 87-91
作者姓名:王艳东  韩智华  蔡君亮  陈晓强  吉庆昌
作者单位:北京航空航天大学自动化科学与电气工程学院,北京,100191
摘    要:
编队飞行中需要确定主机和从机之间的相对位置关系,就是要解决导航定位问题。针对无人机在编队飞行过程中由于机动性较大,惯性元器件测量容易出现偏差,进而影响系统的运动状态方程的情况,或者是在系统噪声与观测噪声的统计特性不能够准确得到的情况,提出了一种新的模糊自适应滤波方法。根据实时得到的量测新息的实际方差与理论方差的差值和量测新息的均值,按照判定条件选择适合的滤波方法,然后由设计的模糊推理系统在线实时调整系统噪声和量测噪声矩阵,或是调整状态误差协方差阵即强跟踪滤波,使无人机编队飞行即使在恶劣的环境下依然保持确定的队形不变。仿真结果表明,该算法具有较好的自适应效果。

关 键 词:相对导航  编队飞行  INS/GPS  模糊自适应滤波  四元数
收稿时间:2011-07-30

A New Fuzzy Adaptive Filtering for Relative Navigation System
WANG Yandong , HAN Zhihua , CAI Junliang , CHEN Xiaoqiang , JI Qingchang. A New Fuzzy Adaptive Filtering for Relative Navigation System[J]. Electronics Optics & Control, 2012, 19(10): 87-91
Authors:WANG Yandong    HAN Zhihua    CAI Junliang    CHEN Xiaoqiang    JI Qingchang
Affiliation:(School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China)
Abstract:
In UAV formation flight,the relative position of the lead aircraft and follower needs to determined,which is to solve the navigation problem.Since the UAV has great maneuverability during formation flight,the inertial measurement components prone to having bias that may affect the motion state equations of the system.Sometimes statistical properties of the system noise and observation noise can not be obtained accurately.To solve the problems,an improved adaptive filtering method was proposed.According to the difference of the actual covariance of real-time measurement and the theoretical covariance,and the mean of the measurement values,an appropriate filtering method was selected based on the conditions.Then,the designed fuzzy inference systems was used to adjust the system noise matrix and the measurement noise matrix,or adjust the state error covariance matrix,thus the UAV formation flight could keep the original formation even under harsh environment.Simulation results show that the algorithm has fine adaptability.
Keywords:relative navigation  formation flight  INS/GPS  FLAS  quaternion
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