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

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

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 orde...

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Bibliographic Details
Main Author: Tamer Mekky Ahmed Habib
Format: Article
Language:English
Published: Elsevier 2013-06-01
Series:Egyptian Journal of Remote Sensing and Space Sciences
Subjects:
Orbit
Control
Estimation
EKF
GPS
Drag
Random disturbance
Online Access:http://www.sciencedirect.com/science/article/pii/S1110982312000270

Internet

http://www.sciencedirect.com/science/article/pii/S1110982312000270

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