Initial inertial navigation alignment method based on terated strong tracking spherical simplex radial cubature Kalman filter (ISTSSRCKF)
A technology of initial alignment and inertial navigation, applied in the field of navigation, which can solve problems such as poor ability to deal with uncertain factors, low alignment accuracy, and inability to filter.
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[0114] The present invention will be further described below in conjunction with the accompanying drawings.
[0115] Step 1: Establish the SINS shaking base alignment model under the state of large misalignment angle, the alignment model includes the nonlinear error model of SINS, the nonlinear filter state model and the nonlinear filter measurement model:
[0116] Among them, the process of establishing the SINS nonlinear error model is as follows:
[0117] Step 1.1: Take the northeast sky geographic coordinate system as the navigation coordinate system n, take the carrier coordinate system b as the carrier coordinate system b with the vector right-hand rule of the right front and upper direction vector, and the real attitude angle is The real speed is v s n = v e n ...
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