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半捷联图像寻的制导系统导引信息构造方法
引用本文:宋建梅,孔丽霞,范健华.半捷联图像寻的制导系统导引信息构造方法[J].兵工学报,2010,31(12):1573-1579.
作者姓名:宋建梅  孔丽霞  范健华
作者单位:北京理工大学,宇航学院,北京,100081;北京理工大学,宇航学院,北京,100081;北京理工大学,宇航学院,北京,100081
摘    要:半捷联导引头的动力学数学模型非线性比较严重,EKF(Extended Kalman Filter)滤波不能满足高精度制导要求。本文采用UKF(Uncented Kalman Filter)滤波方法对框架角速率进行估计,同时结合弹上IMU测量得到的弹体角速率信息以及图像探测器处理得到的目标在像平面上的位置信息,构造导弹的准比例导引信息。通过仿真对比了基于EKF和UKF的框架角速度滤波估计精度,进行了基于UKF的导弹三维飞行仿真。结果表明,基于UKF滤波方法所构造的制导信息精度较高,能够满足导弹精确打击需求。

关 键 词:飞行器控制与导航  半捷联图像寻的  制导信息  EKF  UKF  导弹制导

The Guidance Information Reconstruction of Semi-strapdown Imaging Seeker Guidance System
SONG Jian-mei,KONG Li-xia,FAN Jian-hua.The Guidance Information Reconstruction of Semi-strapdown Imaging Seeker Guidance System[J].Acta Armamentarii,2010,31(12):1573-1579.
Authors:SONG Jian-mei  KONG Li-xia  FAN Jian-hua
Affiliation:(School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China)
Abstract:As the semi-strapdown seeker's dynamics is seriously nonlinear, EKF (Extended Kalman Filter) for guidance information reconstruction can not meet the requirements of high accuracy guidance. This paper uses UKF (Uncented Kalman Filter) to estimate the gimbal angular rate, and at the same time, the quasi-proportional guidance information was reconstructed by combining missile attitude rate coming from IMU with the target position information coming from seeker's imaging plane. The paper finally makes a three-...
Keywords:control and nasigation technology of aerocraft  semi-strapdown imaging seeker  guidance information  extended Kalman filter  unscented Kalman filter  missile guidance  
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