Nonlinear-model-based SINS/DVL (strapdown inertial navigation system/doppler velocity log) integrated navigation method
A nonlinear model and integrated navigation technology, which is applied in the field of navigation, can solve the problems of reduced accuracy of position and velocity estimation, inability to accurately describe the change of the nonlinear characteristic SINS attitude error of the integrated navigation system, etc.
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[0074] The technical solutions of the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0075] A kind of SINS / DVL integrated navigation method based on nonlinear model, it is realized by the following steps:
[0076] Step 1: To establish the nonlinear error model of SINS, first define the navigation coordinate system to be used as follows:
[0077] i——inertial coordinate system
[0078] e—Earth coordinate system
[0079] b——carrier coordinate system
[0080] p - calculated platform coordinate system
[0081] n——Navigation coordinate system that coincides with the Northeast Heaven geographic coordinate system
[0082] Through the speed differential equation of the ideal inertial navigation specific force equation and the actual speed differential equation of the strapdown system, the speed error equation represented by the quaternion can be derived:
[0083] δ ...
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