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快速传递对准的联邦滤波器设计

顾冬晴 秦永元 彭蓉 李欣

南京航空航天大学学报(英文版)2005,Vol.22Issue(2):139-143,5.
南京航空航天大学学报(英文版)2005,Vol.22Issue(2):139-143,5.

快速传递对准的联邦滤波器设计

RAPID TRANSFER ALIGNMENT USING FEDERATED KALMAN FILTER

顾冬晴 1秦永元 1彭蓉 1李欣2

作者信息

  • 1. 西北工业大学自动化学院,西安,710072,中国
  • 2. 海军航空装备论证研究所,上海,200436,中国
  • 折叠

摘要

Abstract

The dimension number of the centralized Kalman filter (CKF) for the rapid transfer alignment (TA) is as high as 21 if the aircraft wing flexure motion is considered in the rapid TA. The 21-dimensional CKF brings the calculation burden on the computer and the difficulty to meet a high filtering updating rate desired by rapid TA. The federated Kalman filter (FKF) for the rapid TA is proposed to solve the dilemma. The structure and the algorithm of the FKF, which can perform parallel computation and has less calculation burden, are designed. The wing flexure motion is modeled, and then the 12-order velocity matching local filter and the 15-order attitude matching local filter are devised. Simulation results show that the proposed FKF for the rapid TA almost has the same performance as the CKF. Thus the calculation burden of the proposed FKF for the rapid TA is markedly decreased.

关键词

快速传递对准/联邦滤波器/机翼挠曲

Key words

rapid transfer alignment/federated Kalman filter/wing flexure

分类

交通工程

引用本文复制引用

顾冬晴,秦永元,彭蓉,李欣..快速传递对准的联邦滤波器设计[J].南京航空航天大学学报(英文版),2005,22(2):139-143,5.

南京航空航天大学学报(英文版)

1005-1120

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