Simultaneous spacecraft orbit estimation and control based on GPS measurements via extended Kalman filter

被引：6

作者：

Habib, Tamer Mekky Ahmed ^{[1
]}

机构：

[1] Egyptian Natl Author Remote Sensing & Space Sci, Cairo, Egypt

来源：

EGYPTIAN JOURNAL OF REMOTE SENSING AND SPACE SCIENCES | 2013年 / 16卷 / 01期

关键词：

Orbit; Control; Estimation; EKF; GPS; Drag; Random disturbance;

D O I：

10.1016/j.ejrs.2012.11.002

中图分类号：

X [环境科学、安全科学];

学科分类号：

08 ; 0830 ;

摘要：

The primary aim of this work is to provide simultaneous spacecraft orbit estimation and control based on the global positioning system (GPS) measurements suitable for application to the next coming Egyptian remote sensing satellites. Disturbance resulting from earth's oblateness till the fourth order (i.e., J(4)) is considered. In addition, aerodynamic drag and random disturbance effects are taken into consideration. (C) 2012 National Authority for Remote Sensing and Space Sciences. Production and hosting by Elsevier B.V. All rights reserved.

引用

页码：11 / 16

页数：6

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