@inproceedings{8547246708e6408e8db732ae18f8a198,
title = "Extension of farrenkopf steady-state solutions with estimated angular rate",
abstract = "Steady-state solutions of the single-axis attitude estimation filter are considered for the traditional case of dynamic model replacement, where the angular rate is determined directly from a gyroscope reading and bias estimate, and for the augmented case where the angular rate is estimated in the filter. The impact of the process noise on the steady-state values is analyzed, and it is found that there exists a value for the process noise below which the augmented filter performs better, and above which the dynamic model replacement filter performs better. A Multiple-Model Adaptive Estimation filter is developed to allow for uncertainties in assumed process noise in the augmented filter to be handled. Three-axis results are compared to single-axis results and are found to perform similarly.",
author = "Dianetti, \{Andrew D.\} and Crassidis, \{John L.\}",
note = "Publisher Copyright: {\textcopyright} 2018 by the American Institute of Aeronautics and Astronautics, Inc.; AIAA Guidance, Navigation, and Control Conference, 2018 ; Conference date: 08-01-2018 Through 12-01-2018",
year = "2018",
month = jan,
day = "1",
doi = "10.2514/6.2018-2095",
language = "English",
isbn = "9781624105265",
series = "AIAA Guidance, Navigation, and Control Conference, 2018",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Guidance, Navigation, and Control",
}