Method of MEMS sensor-based strap-down inertial navigation system (SINS) data preprocessing and attitude calculation
A strapdown inertial navigation and system data technology, applied in the field of sensors and inertial navigation, can solve the problems of cumbersome attitude angle error equation, unfavorable practical use, and increased calculation amount, and achieve the effect of eliminating random noise and suppressing drift error
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[0032] Embodiments of the present invention will be described in detail below. It is illustrated that the present embodiments are illustrative and are only used to explain the present invention, but cannot be construed as limitations of the present invention. A kind of MEMS sensor-based strapdown inertial navigation system data preprocessing and the method for attitude solution of the present invention will be described in detail below with reference to the accompanying drawings:
[0033] like figure 1 As shown, it can be seen that the whole process is mainly divided into two stages: the first stage is the preprocessing of the collected MEMS inertial device data; the second stage is to use the data preprocessed in the first stage, and adopt the attitude fusion algorithm respectively And UKF algorithm for attitude calculation.
[0034] The first stage is to preprocess the data of the inertial device, which is implemented in the following steps:
[0035] 1. To process the data...
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