@inproceedings{47e4675a8c01411681ebcb33bf7f3b2f,
title = "Attitude estimation employing common frame error representations",
abstract = "This work studies vector representation in the attitude filtering problem. Since vector coordinates must be estimated in lieu of the abstract vector itself, the choice of repre- sentation is important. A challenge arises in attitude estimation when the coordinates of a vector are sought with respect to the attitude state coordinate frame. While a wealth of research examines filtering with attitude state constraints or discontinuities, this work focuses on vector state estimation with respect to the attitude state frame. Specifically, an alternative vector state error is defined using common coordinates over all vector error realizations. A modified extended Kalman Filter is developed with this error realization as its foundation. Numerical simulations are conducted, and results obtained using the new filter are compared with those generated by employing a standard estimate error definition.",
author = "Andrle, \{Michael S.\} and Crassidis, \{John L.\}",
note = "Publisher Copyright: {\textcopyright} 2016 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Guidance, Navigation, and Control Conference, 2016 ; Conference date: 04-01-2016 Through 08-01-2016",
year = "2016",
doi = "10.2514/6.2016-0625",
language = "English",
isbn = "9781624103896",
series = "2016 AIAA Guidance, Navigation, and Control Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Guidance, Navigation, and Control Conference",
}