Small satellite attitude control based on a Kalman filter

被引：6

作者：

Clements, R ^{[1
]}

Tavares, P ^{[1
]}

Lima, P ^{[1
]}

机构：

[1] Univ Tecn Lisboa, Inst Sistemas & Robot, Inst Super Tecn, P-1049001 Lisbon, Portugal

来源：

PROCEEDINGS OF THE 2000 IEEE INTERNATIONAL SYMPOSIUM ON INTELLIGENT CONTROL | 2000年

关键词：

extended Kalman filter; genetic algorithms; sun sensor; magnetometer; small satellites;

D O I：

10.1109/ISIC.2000.882903

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper 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.

引用

页码：79 / 84

页数：6

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