Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor

Kinatas, Hasan; Hajiyev, Chingiz

Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor

Hasan Kinatas, (İstanbul Teknik Üniversitesi, Havacılık ve Uzay Bilimleri Fakültesi, İstanbul, Türkiye)

Chingiz Hajiyev (İstanbul Teknik Üniversitesi, Havacılık ve Uzay Bilimleri Fakültesi, İstanbul, Türkiye)

Havacılık ve Uzay Teknolojileri Dergisi

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Yıl: 2022 Cilt: 15 Sayı: 2 Sayfa Aralığı: 74 - 93 Metin Dili: İngilizce İndeks Tarihi: 08-09-2022

Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor

Öz:

In this study, an integrated adaptive TRIAD/Extended Kalman Filter (EKF) attitude estimation system is presented, in which the TRIAD and an adaptive EKF are combined to estimate the attitude of a nanosatellite. As the first step of the system, the TRIAD algorithm produces an initial coarse quaternion estimation by using magnetometer and sun sensor measurements, and then, this coarse estimation is directly fed to the adaptive EKF. This direct input of the attitude information to the filter relatively reduces the computational burden that an EKF brings. As the second step of the system, adaptive EKF filters the TRIAD solution and gives the final quaternion estimation. At the same time, the adaptive EKF readjusts the measurement noise covariance matrix by using a single scaling factor (SSF) in case of a sensor fault and makes the overall system more robust against the sensor malfunctions. Several simulations are performed, and the performance of the presented system is tested against two different fault types as noise increment and continuous bias in attitude sensors.

Anahtar Kelime: Nanosatellite attitude estimation adaptive Kalman filtering fault magnetometer sun sensor

Tek Ölçekleme Faktörlü Uyarlanabilir Kalman Filtresi Kullanarak Bir Nanouydu için Hata Toleranslı Yönelim Tahmini

Öz:

Bu çalışmada, bir nanouydunun yönelimini tahmin etmek için TRIAD ve uyarlamalı bir genişletilmiş Kalman süzgeci (GKS) algoritmasının birleştirildiği entegre bir uyarlamalı TRIAD/GKS yönelim tahmin algoritması sunulmaktadır. TRIAD tarafından manyetometre ve güneş sensörü ölçümleri kullanılarak üretilen kuaterniyon seti, uyarlanabilir GKS'ye girdi olarak sağlanır. Böylece GKS’nin sisteme getirmiş olduğu hesaplama yükü nispeten azaltılmış olur. Daha sonra uyarlanabilir GKS, TRIAD çözümündeki gürültüyü azaltarak nihai kuaterniyon setini verir. Uyarlanabilir GKS aynı zamanda tek ölçekleme faktörü (TÖF) kullanarak, yönelim sensörlerinde oluşabilecek bir hata durumunda ölçüm gürültüsü kovaryans matrisini yeniden ayarlayarak süzgeci arızalara karşı daha dirençli hale getirir. Önerilen entegre sistemin performansı, yönelim sensörlerinde devamlı bayas olması ya da sensör gürültülerinin aniden artması durumlarına karşı çeşitli benzetimlerle test edilmiştir.

Anahtar Kelime:

Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık

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APA	Kinatas H, Hajiyev C (2022). Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. , 74 - 93.
Chicago	Kinatas Hasan,Hajiyev Chingiz Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. (2022): 74 - 93.
MLA	Kinatas Hasan,Hajiyev Chingiz Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. , 2022, ss.74 - 93.
AMA	Kinatas H,Hajiyev C Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. . 2022; 74 - 93.
Vancouver	Kinatas H,Hajiyev C Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. . 2022; 74 - 93.
IEEE	Kinatas H,Hajiyev C "Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor." , ss.74 - 93, 2022.
ISNAD	Kinatas, Hasan - Hajiyev, Chingiz. "Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor". (2022), 74-93.

APA	Kinatas H, Hajiyev C (2022). Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. Havacılık ve Uzay Teknolojileri Dergisi, 15(2), 74 - 93.
Chicago	Kinatas Hasan,Hajiyev Chingiz Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. Havacılık ve Uzay Teknolojileri Dergisi 15, no.2 (2022): 74 - 93.
MLA	Kinatas Hasan,Hajiyev Chingiz Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. Havacılık ve Uzay Teknolojileri Dergisi, vol.15, no.2, 2022, ss.74 - 93.
AMA	Kinatas H,Hajiyev C Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. Havacılık ve Uzay Teknolojileri Dergisi. 2022; 15(2): 74 - 93.
Vancouver	Kinatas H,Hajiyev C Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor. Havacılık ve Uzay Teknolojileri Dergisi. 2022; 15(2): 74 - 93.
IEEE	Kinatas H,Hajiyev C "Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor." Havacılık ve Uzay Teknolojileri Dergisi, 15, ss.74 - 93, 2022.
ISNAD	Kinatas, Hasan - Hajiyev, Chingiz. "Fault Tolerant Attitude Estimation for a Nanosatellite Using Adaptive Kalman Filter with Single Scaling Factor". Havacılık ve Uzay Teknolojileri Dergisi 15/2 (2022), 74-93.