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Design and Simulation of Autonomous Control System of Satellite
Beijing, China August 30-September 01
DOI Bookmark: http://doi.ieeecomputersociety.org/10.1109/ICICIC.2006.66First International Conference on Inn ...
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Xiang Junhua, Zhang Yulin, "Design and Simulation of Autonomous Control System of Satellite," Innovative Computing ,Information and Control, International Conference on, vol. 1, pp. 109-112, First International Conference on Innovative Computing, Information and Control - Volume I (ICICIC'06), 2006.
 
 
BibTex
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@article{ 10.1109/ICICIC.2006.66,
author = {Xiang Junhua and Zhang Yulin},
title = {Design and Simulation of Autonomous Control System of Satellite},
journal ={Innovative Computing ,Information and Control, International Conference on},
volume = {1},
year = {2006},
isbn = {0-7695-2616-0},
pages = {109-112},
doi = {http://doi.ieeecomputersociety.org/10.1109/ICICIC.2006.66},
publisher = {IEEE Computer Society},
address = {Los Alamitos, CA, USA},
}
 
 
RefWorks Procite/RefMan/Endnote
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TY - CONF
JO - Innovative Computing ,Information and Control, International Conference on
TI - Design and Simulation of Autonomous Control System of Satellite
SN - 0-7695-2616-0
SP109
EP112
A1 - Xiang Junhua,
A1 - Zhang Yulin,
PY - 2006
KW - null
VL - 1
JA - Innovative Computing ,Information and Control, International Conference on
ER -
 
Zhang Yulin, Tsinghua University
Analyzed the influence of main perturbation sources including non-spherical gravitational perturbation, atmospheric drag perturbation and third body gravitation perturbation to the satellite orbit, compensates the influence through the method that biased the semi-major axis and the inclination angle, which enhanced the orbital stability of satellite. Designed the satellite autonomous orbital control system, and discussed the method that through controlling the semi-major axis, the eccentricity and the inclination angle to complete the revisions to ascending node right ascension deviation and phase deviation. Finally through the simulation and the experiment of a satellite which running on nearly earth regression, circular orbit, simulation results indicated the system scheme satisfied the demand of satellite autonomous control.
Citation:
Xiang Junhua, Zhang Yulin, "Design and Simulation of Autonomous Control System of Satellite," icicic, vol. 1, pp.109-112, First International Conference on Innovative Computing, Information and Control - Volume I (ICICIC'06), 2006
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