Attitude Determination of Nanosatellites in the Sun-Eclipse Phases

被引：0

作者：

Hajiyev, Chingiz ^{[1
]}

Cilden-Guler, Demet ^{[1
]}

Somov, Yevgeny ^{[2
]}

机构：

[1] Istanbul Tech Univ, Fac Aeronaut & Astronaut, Istanbul, Turkey

[2] Samara State Tech Univ, Dept Guidance Nav & Control, Samara, Russia

来源：

PROCEEDINGS OF 8TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2017) | 2017年

基金：

俄罗斯基础研究基金会;

关键词：

Satellite attitude estimation; magnetometer; sun sensor; rate gyro; extended Kalman filter; attitude prediction; KALMAN FILTER; DESIGN;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Singular Value Decomposition (SVD) and extended Kalman filter (EKF) are integrated earlier by authors in order to estimate the satellite's angular motion parameters about center of mass. The SVD-aided EKF algorithm is used in this study for estimation of the attitude angles and angular velocities. In the eclipse period, algorithm is switched into the prediction phase for better attitude estimation of the satellite; therefore, satellite's attitude angles when no data coming from the sun sensor are improved.

引用

页码：397 / 401

页数：5

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