Method and system for improving indoor inertial navigation precision
An inertial navigation and precision technology, applied in the field of navigation, can solve problems such as many sources of interference, restrictions on popularization of technology, expensive manual processing, etc., and achieve the effect of improving accuracy
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Embodiment 1
[0039] This embodiment provides a method for improving the accuracy of indoor inertial navigation, such as figure 1 shown, including steps:
[0040] S11. Collect the navigation data information of the indoor location;
[0041] S12. Establishing an error model corresponding to the information according to the collected navigation data information;
[0042] S13. Calculate the current location information through an inertial navigation algorithm; the inertial navigation includes inertial navigation parameters;
[0043] S14. Comparing the calculated current location information with the navigation data information in the established error model to obtain a comparison result;
[0044] S15. Correct the parameters of the inertial navigation according to the obtained comparison result.
[0045] This embodiment is described in detail using a WeChat applet in a mobile terminal. It should be noted that this embodiment is not limited to the application of WeChat applets, and this embo...
Embodiment 2
[0088] This embodiment provides a system for improving the accuracy of indoor inertial navigation, such as figure 2 shown, including:
[0089] Acquisition module 11, for collecting the navigation data information of indoor position;
[0090] Establishment module 12, is used for establishing the error model corresponding to described information according to the navigation data information collected;
[0091] Calculation module 13, is used for calculating the current position information by the algorithm of inertial navigation; Said inertial navigation includes the parameter of inertial navigation;
[0092] A comparison module 14, configured to compare the calculated current location information with the navigation data information in the established error model to obtain a comparison result;
[0093] The correction module 15 is configured to correct the parameters of the inertial navigation according to the obtained comparison result.
[0094] This embodiment is described ...
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