In-situ Calibration Technology Approach for the Ship-launched Missile Strapdown Inertial Navigation System
Abstract：According to the ship-luanehed missile SINS, a in-situ calibration scheme is presented in this paper. This scheme can calibrate inertial instrument errors with the velocity and attitude information provided by stapdown attitude and heading reference system, and it dosen＇t need the test equipment such as turntable and dismantling the SINS from missile. The simulation results show that the new method can calibrate avaliably the errors of missile SINS with acceptable precision and therefore it has practical significance.
Keywords：strapdown inertial navigation systemin-situ calibrationstrapdown attitude and heading reference system
Publication Date：2011-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：4( 47-49,59 )