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运载火箭飞行测量数据奇异点检测和降噪处理的小波方法
引用本文:樊友平,陈允平,柴毅,黄席樾,韩逢庆,高波.运载火箭飞行测量数据奇异点检测和降噪处理的小波方法[J].宇航学报,2005,26(5):591-599,624.
作者姓名:樊友平  陈允平  柴毅  黄席樾  韩逢庆  高波
作者单位:1. 武汉大学电气工程学院,武汉,430072;重庆大学自动化学院,重庆,400044
2. 武汉大学电气工程学院,武汉,430072
3. 重庆大学自动化学院,重庆,400044
4. 西昌卫星发射中心,西昌,615000
基金项目:国防预研基金资助(2000264);中国博士后科学基金(2004036135)
摘    要:以提高火箭飞行测量数据处理精度为主要目的,结合弹道处理的实际,将小波理论运用于火箭弹道测量数据的分析。首先,在对信号奇异性、小波方法检测信号奇异点原理探讨的基础上,通过对火箭飞行外弹道测量数据奇异性的分析,确定了用于火箭飞行数据奇异点检测的小波函数的选取原则,提出了对跟踪测量数据奇异性点准确定位和分析其奇异性类型的方法;其次,为提高处理火箭飞行弹道的光滑度,深入探讨了弹道测量数据的小波消噪方法,结合雷达跟踪测量数据的实际分析和处理情况,就数据是否处于火箭在级间分离段提出了不同的处理方法。该算法原理简捷,计算复杂度较低,易实现。最后,通过对某试测的两个测量站雷达弹道测量数据的分析处理,论证了上述方法的正确性,取得了明显的效果。

关 键 词:信号处理  小波变换  奇异信号  运载火箭
文章编号:1000-1328(2005)05-0591-09
收稿时间:2004-05-27
修稿时间:2004-05-272004-11-10

Research on Processing Method of Singularity Detection and Noise Elimination Based on Wavelet Transform for Data Measured in Launch Vehicle Aviation
FAN You-ping,CHEN Yun-ping,CHAI Yi,HUANG Xi-yue,HAN Feng-qing,GAO Bo.Research on Processing Method of Singularity Detection and Noise Elimination Based on Wavelet Transform for Data Measured in Launch Vehicle Aviation[J].Journal of Astronautics,2005,26(5):591-599,624.
Authors:FAN You-ping  CHEN Yun-ping  CHAI Yi  HUANG Xi-yue  HAN Feng-qing  GAO Bo
Institution:1. Electrical Engineering College, Wuhan University, Hubei. Prov. Wuhan 430072, China; 2. Automation College, Chongqing University, Chongqing400044, China; 3. XiChang Satellite Launching Center, XiChang 615000, China
Abstract:The paper presents to enhance the accuracy of rocket aviation tracking data processing in launching site by applying the Wavelet transform to processing of rocket launching trajectory data measured based on the real launching experiment. Firstly, setting the principle of selecting the wavelet function in detecting rocket aviation signal singularity, put forward the methods of real time confirmation of the singularity and the exact position of measured data as well as analyzing the singularity types. Secondly, explored the Wavelet noise elimination method of trajectory-|measured data to improve the smoothness of rocket aviation trajectory and put up a new simplification algorithm of noise elimination for if the data in rocket stage separating sect based on the practice of trajectory processing. Finally, with the goal of correct orientation of tracking data singularity and analysis of singularity types achieved, the analysis of a real case of processing of radar trajectory measured data in the mission proved the correctness and the effectiveness of above method.
Keywords:Signal processing  Wavelet transform  Singular signals  Launch vehicle
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