The error estimate to the single circle observation data of satellite

Zhuanmin Zhu; Hongxing Qiu; Zongben Xu

The error estimate to the single circle observation data of satellite

Translated title of the contribution: The error estimate to the single circle observation data of satellite

Zhuanmin Zhu
, Hongxing Qiu
, Zongben Xu

School of Mathematics and Statistics

Research output: Contribution to journal › Article › peer-review

Abstract

Through building up an exact dynamics model of the object, a method based on the orbit precise determination and forecast to distinguish and eliminate the error is proposed. It gets over the limitation of the polynomial imitate method which distinguish the error by error effectively.

Translated title of the contribution	The error estimate to the single circle observation data of satellite
Original language	Chinese (Traditional)
Pages (from-to)	29-33
Number of pages	5
Journal	Chinese Space Science and Technology
Volume	25
Issue number	5
State	Published - Oct 2005

Cite this

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title = "The error estimate to the single circle observation data of satellite",

abstract = "Through building up an exact dynamics model of the object, a method based on the orbit precise determination and forecast to distinguish and eliminate the error is proposed. It gets over the limitation of the polynomial imitate method which distinguish the error by error effectively.",

keywords = "Error analysis, Orbit determination, Satellite observation",

author = "Zhuanmin Zhu and Hongxing Qiu and Zongben Xu",

year = "2005",

month = oct,

language = "繁体中文",

volume = "25",

pages = "29--33",

journal = "Chinese Space Science and Technology",

issn = "1000-758X",

publisher = "Chinese Academy of Space Technology",

number = "5",

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T1 - The error estimate to the single circle observation data of satellite

AU - Zhu, Zhuanmin

AU - Qiu, Hongxing

AU - Xu, Zongben

PY - 2005/10

Y1 - 2005/10

N2 - Through building up an exact dynamics model of the object, a method based on the orbit precise determination and forecast to distinguish and eliminate the error is proposed. It gets over the limitation of the polynomial imitate method which distinguish the error by error effectively.

AB - Through building up an exact dynamics model of the object, a method based on the orbit precise determination and forecast to distinguish and eliminate the error is proposed. It gets over the limitation of the polynomial imitate method which distinguish the error by error effectively.

KW - Error analysis

KW - Orbit determination

KW - Satellite observation

UR - https://www.scopus.com/pages/publications/29544442738

M3 - 文章

AN - SCOPUS:29544442738

SN - 1000-758X

VL - 25

SP - 29

EP - 33

JO - Chinese Space Science and Technology

JF - Chinese Space Science and Technology

IS - 5

ER -

The error estimate to the single circle observation data of satellite

Abstract

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