@inproceedings{Carvalho2009Inertialb,

title = {GPS-aided inertial navigation performance evaluation using the Extended Kalman Filter},

author = {Carvalho and F M R Bruno and M G S Carvalho and R T},

url = {https://www.sige.ita.br/edicoes-anteriores/2009/st/VIII_2.pdf},

year  = {2009},

date = {2009-01-01},

booktitle = {Simp\'{o}sio de Aplica\c{c}\~{o}es Operacionais em \'{A}reas de Defesa 2009 (SIGE2009)},

abstract = {We discuss the performance of a GPS-aided inertial navigation system that employs the Extended Kalman Filter (EKF) and GPS position measurements for estimating and correcting position errors on the inertial navigation system readings. A proper error model to account for position, velocity and attitude errors is described and validate. It also estimates the bias drift of both accelerometers and gyrometers, and GPS clock bias. Results on the EKF performance are presented for different flight trajectories. Key words Inertial Navigation, GPS, Kalman Filter.},

keywords = {GPS, Inertial Navigation, Kalman Filter},

pubstate = {published},

tppubtype = {inproceedings}

}