Heave measurement method based on carrier attitude information
A technology of attitude information and measurement methods, applied in the field of measurement, can solve problems such as heavy workload of filter parameter debugging, inability to collect GPS signals, and error divergence of inertial navigation systems
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[0061] One of the core ideas of the present invention is to determine the characteristics of the carrier fluctuating with the waves by analyzing the frequency spectrum characteristics of the carrier attitude information. Adaptively adjust the filter parameters according to the fluctuation characteristics to realize the filter design. The vertical acceleration information of the carrier is obtained through the principle of the inertial navigation system, and then the heave motion information of the carrier is obtained after three times of filtering and two times of integration.
[0062] Below in conjunction with accompanying drawing and specific example the present invention will be described in further detail:
[0063] refer to figure 1 , shows a flow chart of the steps of a heave measurement method based on carrier attitude information in an embodiment of the present invention. In this embodiment, the heave measurement method of the carrier attitude information includes:
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