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- W2785899138 abstract "To the problems of temperature drift in MEMS pressure sensor, inaccuracy of pressure altitude model and noises in height measurement, the temperature compensation, modeling and fusion with inertial navigation system in altitude measurement are studied. Firstly, the pressure error due to temperature is analyzed and compensated. Secondly, numerical integration is applied in altitude computation, which is compared with standard atmosphere altitude model. Finally, information fusion based on INS and pressure sensors is realized by Adaptive Filter. Experiment shows that the altitude and vertical velocity measurement with this method is accurate, swift and free of error accumulation." @default.
- W2785899138 created "2018-02-23" @default.
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- W2785899138 date "2017-12-01" @default.
- W2785899138 modified "2023-09-24" @default.
- W2785899138 title "Research of altitude measurement method based on INS and pressure sensor" @default.
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- W2785899138 doi "https://doi.org/10.1109/itnec.2017.8285082" @default.
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