FIELD: instrumentation engineering. SUBSTANCE: two inertial navigation systems are connected through their outputs to inputs of computer whose other inputs are connected to satellite navigation system and altimeter. Computer uses Kalman filter and binary filter. Speed and vertical position error estimates picked off filter output are passed to inertial navigation system for error correction. EFFECT: improved measurement accuracy. 8 cl, 1 dwg, 1 tbl
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Authors
Dates
2000-05-27—Published
1998-10-30—Filed