发明名称 INERTIAL NAVIGATION SYSTEM
摘要 PROBLEM TO BE SOLVED: To reduce error in the estimated value of fixing error caused by distortion of hull by weighting an estimated angular speed obtained through an inertial navigation system and a main inertial navigation system mounted on a sailing body and setting the angular speed difference of error covariance of the observation disturbance vector of a Kalman filter larger than a standard value. SOLUTION: At the time of estimating a fixing error around Z axis through an inertial navigation system, an angular speed estimated based on X angular speed difference is weighted as compared with that based on Y angular speed difference obtained through a master INS 10 and a sailing body INS 20. X and Y angular speed differences of a matrix RE satisfy a relationship; RE (X angular speed) <RE (Y angular speed difference). At the time of estimating a fixing error through a Kalman filter, a plurality of parameters are selected and weighted as observation values. Extent of weighting of estimation is distributed to minimize the error caused by distortion of hull contained in the fixing error. Extent of each state vector is represented by Kalman gain from observation values. Subsequently, initial value of error covariance matrix, covariance matrix of system disturbance vector error, and the like, are set.
申请公布号 JPH11281300(A) 申请公布日期 1999.10.15
申请号 JP19980086499 申请日期 1998.03.31
申请人 TECH RES & DEV INST OF JAPAN DEF AGENCY;TOKIMEC INC 发明人 TAKAGI MAMORU;TANAKA KOICHI;TAKEUCHI SHUNKICHI;NAMIKI SHINICHI;HITOMI AKIRA
分类号 F42B19/00;B64C13/18;F41G7/36;F42B15/01;G01C21/16;G05D1/12;(IPC1-7):F42B19/00 主分类号 F42B19/00
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