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基于知识神经网络的运载火箭弹道选择
引用本文:魏洪波,黄席樾,乔宇,李娅,李伟. 基于知识神经网络的运载火箭弹道选择[J]. 重庆大学学报(自然科学版), 2005, 28(11): 27-30
作者姓名:魏洪波  黄席樾  乔宇  李娅  李伟
作者单位:西昌卫星发射中心,四川,西昌,615000;重庆大学,自动化学院导航与制导研究所,重庆,400030
摘    要:在火箭发射中,往往有多组来自不同设备的测量弹道,进行可靠的火箭弹道选择是飞行状态监视和安控判断的前提.考虑到火箭飞行过程和测量环境的复杂性,提出了一种基于知识神经网络的运载火箭弹道选择方法.把火箭飞行弹道的先验知识和弹道样本的学习训练相结合,先利用数据的连续性排除跳变弹道,然后计算弹道间的差异,最后采用一个神经网络判断各条弹道的可靠性,并结合测量设备精度进行选优.实验和仿真表明了这种方法的可靠性和有效性.

关 键 词:神经网络  弹道选择  火箭安控系统
文章编号:1000-582X(2005)11-0027-04
收稿时间:2005-06-02
修稿时间:2005-06-02

Craft Orbit Selection by Knowledge Based Neural Network
WEI Hong-bo,HUANG Xi-yue,QIAO Yu,LI Y,LI Wei. Craft Orbit Selection by Knowledge Based Neural Network[J]. Journal of Chongqing University(Natural Science Edition), 2005, 28(11): 27-30
Authors:WEI Hong-bo  HUANG Xi-yue  QIAO Yu  LI Y  LI Wei
Affiliation:1. Xichang Satellite Launching Center, Xichang 615000, China; 2. College of Automation, Chongqing University, Chongqing 400030, China
Abstract:There are more than one measure devices during the craft launching proceeding, reliable craft orbit measurement selection is important for launching monitor and safety control. This paper proposes a novel orbit selection method by knowledge based neural network, which combines the human knowledge and orbit samples based training together. The false spur orbit data are deleted according the data continuity rule at first, then the difference between orbit data is computed, and at last a neural network is trained to test reliability of each data and select the orbit with high precision among all orbit data. Simulations and experiments show the efficiency and reliability of our method.
Keywords:neural network   orbit selection   craft safety control system
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