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A Research on the Way of EMBET in the Tracking Systems'' Accuracy-analysis During Satellite Launch
引用本文:GAO Bo,HUANG Xi yue,YU Wang qing,CHE Zhu ming. A Research on the Way of EMBET in the Tracking Systems'' Accuracy-analysis During Satellite Launch[J]. 保鲜与加工, 2002, 0(1): 88-91
作者姓名:GAO Bo  HUANG Xi yue  YU Wang qing  CHE Zhu ming
摘    要:In the past, the criterion for calibration has almost invariably been the stellar oriented ballistic camera,the method is a point to point comparison on the identical coordinate system. Deficiencies is follows: The request of weather is severe(cloudless night); The period is often long; the measure equipment of high precision can't be calibrated. While EMBET methods is used in calibration, it does not need criterion and it demands only that the measure elements is larger than 3,and the trajectory and many system errors of the measure elements can be simultaneously calculated with the measure data sequences. The error models of related equipments' measure elements and the EMBET of typical equipment group are given. The EMBET method is successfully used in Accuracy-analysis of Satellite Launch.

关 键 词:error model  best estimate  trajectory  calibration
修稿时间:2001-06-02

A Research on the Way of EMBET in the Tracking Systems'' Accuracy-analysis During Satellite Launch
GAO Bo,HUANG Xi yue,YU Wang qing,CHE Zhu ming. A Research on the Way of EMBET in the Tracking Systems'' Accuracy-analysis During Satellite Launch[J]. Storage & Process, 2002, 0(1): 88-91
Authors:GAO Bo  HUANG Xi yue  YU Wang qing  CHE Zhu ming
Abstract:In the past, the criterion for calibration has almost invariably been the stellar oriented ballistic camera,the method is a point to point comparison on the identical coordinate system. Deficiencies is follows: The request of weather is severe(cloudless night); The period is often long; the measure equipment of high precision can't be calibrated. While EMBET methods is used in calibration, it does not need criterion and it demands only that the measure elements is larger than 3,and the trajectory and many system errors of the measure elements can be simultaneously calculated with the measure data sequences. The error models of related equipments' measure elements and the EMBET of typical equipment group are given. The EMBET method is successfully used in Accuracy-analysis of Satellite Launch.
Keywords:error model  best estimate  trajectory  calibration
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