Research Article

A Preferable Airborne Integrated Navigation Method Based on INS and GPS

Table 6

Observable error estimation status of IMU.

Observable errorTest valueEstimated valueAccuracy of estimation

1°/h1.1°/h91%
1°/h1.1°/h91%
1°/h0.5°/h50%
300 ppm327 ppm90%
300 ppm214 ppm71%
405178%
403895%
40−4393%
500 μg602 μg83%
500 μg702 μg71%
500 μg107 μg21%
300 ppm369 ppm81%
300 ppm62 ppm21%
401333%
40−820%