Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Ece Sevim Conguroglu"'
Publikováno v:
Metrology and Measurement Systems, Vol 24, Iss 2, Pp 313-324 (2017)
Single-frame methods of determining the attitude of a nanosatellite are compared in this study. The methods selected for comparison are: Single Value Decomposition (SVD), q method, Quaternion ESTimator (QUEST), Fast Optimal Attitude Matrix (FOAM) −
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9bf9e4988e1547b5ecb1529bf0d01148
https://doi.org/10.1515/mms-2017-0023
https://doi.org/10.1515/mms-2017-0023
Autor:
Ece Sevim Conguroglu, Chingiz Hajiyev
Publikováno v:
2015 7th International Conference on Recent Advances in Space Technologies (RAST).
In this study an integrated Algebraic method/ Extended Kalman fitler (EKF) attitude determination system is presented, in which the 2-vector and EKF algorithms are combined to estimate the attitude angles and angular velocities. As a reference direct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f380ba8387c5827684248c48a337eb20
https://doi.org/10.1109/rast.2015.7208435
https://doi.org/10.1109/rast.2015.7208435
Publikováno v:
2015 7th International Conference on Recent Advances in Space Technologies (RAST).
Two different methods are compared to estimate attitude in this study. These methods are Single Value Decomposition (SVD) solving Wahba's problem optimally and Algebraic Method using two vector measurements. Selected spacecraft data is used for orbit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8bf1d1987085043312219fea07ee0e5
https://doi.org/10.1109/rast.2015.7208432
https://doi.org/10.1109/rast.2015.7208432