Browse

The paper presents the evaluation with experimental data of an ANFIS based INS/GPS integrated navigator. The experimental model of the INS/GPS navigator has been manufactured in the Aerospace Engineering laboratories of the University of Craiova, Romania, during a research project. This hardware structure was developed around an inertial module (inertial detection unit) incorporating three analogous miniaturized inertial sensors (LPY510AL - Biaxial analog gyro, LPR510AL - Biaxial analog gyro, MMA7361L ? Three-axia...

The paper exposes the tuning and the evaluation with experimental data of an algorithm used to predict the lost data in the GPS readings due to the acquisition rate significantly different from that of the Inertial Navigation System (INS). The developed algorithm provides a real time prediction of the GPS data at the same rate with the INS data in order to be ready for the processing step, which realizes the fusion of the two systems. To acquire the data, an INS/GPS hardware structure based MEMS sensors has been d...