DocumentCode :
2615015
Title :
Small satellite attitude control based on a Kalman filter
Author :
Clements, Robert ; Tavares, P. ; Lima, Pedro
Author_Institution :
Inst. de Sistemas e Robotica, Inst. Superior Tecnico, Lisbon, Portugal
fYear :
2000
fDate :
2000
Firstpage :
79
Lastpage :
84
Abstract :
Describes the development of an extended Kalman filter attitude estimator and its implementation in a small satellite control loop. Sensor models have first been added to an existing satellite simulation. The attitude and angular velocities are estimated from the available sensors and methods of tuning the filter based on genetic algorithms are discussed. Simulation results are presented for the estimator algorithm used with different control algorithms
Keywords :
Kalman filters; artificial satellites; attitude control; closed loop systems; filtering theory; genetic algorithms; magnetometers; nonlinear filters; optical sensors; angular velocities; estimator algorithm; extended Kalman filter; satellite simulation; sensor models; small satellite attitude control; Attitude control; Extraterrestrial measurements; Genetic algorithms; Magnetic field measurement; Magnetic sensors; Magnetometers; Position measurement; Satellites; Sensor phenomena and characterization; Sun;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control, 2000. Proceedings of the 2000 IEEE International Symposium on
Conference_Location :
Rio Patras
ISSN :
2158-9860
Print_ISBN :
0-7803-6491-0
Type :
conf
DOI :
10.1109/ISIC.2000.882903
Filename :
882903
Link To Document :
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