INS/GPS/MNS Integrated Navigation System with Federated Kalman Filtering
2013 ◽
Vol 718-720
◽
pp. 1207-1212
Keyword(s):
A multi-sensor integrated solution that combine complementary features of the Global Positioning System (GPS), inertial navigation system (INS), and magnetometer is presented due to GPS-aided inertial navigation system (INS) provides poor observability of heading angle. In addition, Based on the principle of federated Kalman filtering and Adaptive Extended Kalman Filter, the algorithm is presented also for accuracy of positioning and attitude, rapidity, and error tolerance of the navigation system. The algorithm is implemented in the integrated navigation system. Experimental results show that the observability issue is solved and improvement in accuracy.
1992 ◽
Vol 97
(B6)
◽
pp. 8853
◽
2010 ◽
Vol 136
(3)
◽
pp. 139-146
◽
2020 ◽
Vol 98
◽
pp. 105679
◽
2013 ◽
Vol 336-338
◽
pp. 277-280
◽
2014 ◽
Vol 711
◽
pp. 338-341
◽
2012 ◽
Vol 433-440
◽
pp. 3175-3180