In-orbit magnetometer calibration based on linear Kalman filtering

Chingiz Hajiyev

In-orbit magnetometer calibration based on linear Kalman filtering

Chingiz Hajiyev^*

^*Bu çalışma için yazışmadan sorumlu yazar

Uçak Mühendisliği Bölümü

Araştırma sonucu: Konferansa katkı › Yazı › bilirkişi

Özet

Magnetometers are widely used for LEO small satellites attitude determination and control system. In order to estimate satellite dynamics and control attitude accurately, scale factor and bias of magnetometer must be estimated. In this study a Linear Kalman filter (LKF) based algorithm for the estimation of magnetometer biases and scale factors is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite.

Orijinal dil	İngilizce
Yayın durumu	Yayınlandı - 2015
Etkinlik	21st IMEKO World Congress on Measurement in Research and Industry - Prague, Czech Republic Süre: 30 Ağu 2015 → 4 Eyl 2015

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???event.eventtypes.event.conference???	21st IMEKO World Congress on Measurement in Research and Industry
Ülke/Bölge	Czech Republic
Şehir	Prague
Periyot	30/08/15 → 4/09/15

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

@conference{cb921e28b7e84a53995b6d7083cc3845,

title = "In-orbit magnetometer calibration based on linear Kalman filtering",

abstract = "Magnetometers are widely used for LEO small satellites attitude determination and control system. In order to estimate satellite dynamics and control attitude accurately, scale factor and bias of magnetometer must be estimated. In this study a Linear Kalman filter (LKF) based algorithm for the estimation of magnetometer biases and scale factors is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite.",

keywords = "Attitude determination, Calibration, Kalman filtering, Magnetometer, Satellite",

author = "Chingiz Hajiyev",

year = "2015",

language = "English",

note = "21st IMEKO World Congress on Measurement in Research and Industry ; Conference date: 30-08-2015 Through 04-09-2015",

}

TY - CONF

T1 - In-orbit magnetometer calibration based on linear Kalman filtering

AU - Hajiyev, Chingiz

PY - 2015

Y1 - 2015

N2 - Magnetometers are widely used for LEO small satellites attitude determination and control system. In order to estimate satellite dynamics and control attitude accurately, scale factor and bias of magnetometer must be estimated. In this study a Linear Kalman filter (LKF) based algorithm for the estimation of magnetometer biases and scale factors is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite.

AB - Magnetometers are widely used for LEO small satellites attitude determination and control system. In order to estimate satellite dynamics and control attitude accurately, scale factor and bias of magnetometer must be estimated. In this study a Linear Kalman filter (LKF) based algorithm for the estimation of magnetometer biases and scale factors is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite.

KW - Attitude determination

KW - Calibration

KW - Kalman filtering

KW - Magnetometer

KW - Satellite

UR - https://www.scopus.com/pages/publications/84951096630

M3 - Paper

AN - SCOPUS:84951096630

T2 - 21st IMEKO World Congress on Measurement in Research and Industry

Y2 - 30 August 2015 through 4 September 2015

ER -

In-orbit magnetometer calibration based on linear Kalman filtering

Özet

???event.eventtypes.event.conference???

Diğer Dosyalar ve Linkler

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