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

In this study an integrated adaptive TRIAD/Extended Kalman Filter (EKF) attitude estimation algorithm is presented, in which the TRIAD and an adaptive EKF are combined to estimate the attitude of a nanosatellite. The quaternion set produced by the TRIAD is provided as input to the adaptive EKF. Adap...

Szczegółowa specyfikacja

Opis bibliograficzny

Główni autorzy:	Hasan Kınataş, Cengiz Hacızade
Format:	Artigo
Język:	Inglês
Wydane:	Turkish Air Force Academy 2022-07-01
Seria:	Havacılık ve Uzay Teknolojileri Dergisi
Hasła przedmiotowe:	nanosatellite, attitude estimation, adaptive kalman filtering, fault, magnetometer, sun sensor
Dostęp online:	https://jast.hho.msu.edu.tr/index.php/JAST/article/view/520
Etykiety:	Dodaj etykietę Nie ma etykietki, Dołącz pierwszą etykiete!