发明名称 NAVIGATION COMPLEX, VELOCITY AND COORDINATES' CALCULATION, GIMBALLESS INERTIAL ATTITUDE-AND-HEADING REFERENCE SYSTEM, CORRECTION METHOD FOR INERTIAL TRANSDUCERS AND DEVICE FOR ITS IMPLEMENTATION
摘要 FIELD: measurement technology. ^ SUBSTANCE: group of inventions refers to the instrument engineering sphere and can be used for gimballess inertial navigation systems of the aircrafts (AC) and, especially, for low-sized unmanned aircrafts (UMAC). To achieve this result the navigation complex contains gimballess inertial attitude-and-heading reference system (GIAHRS), device for calculation of the velocity and coordinates , three-channel block of linear acceleration transducer (LAT), block of coordinates' measurement, three-stage magnetic direction transducer, three-channel block of angular velocities' transducer. Determination of the angular attitude vector, velocity vector and radius-vector is realised by measuring the angular attitude vector and linear acceleration vector by automatic combination controller. ^ EFFECT: invention improves the accuracy. ^ 12 cl, 7 dwg
申请公布号 RU2373498(C2) 申请公布日期 2009.11.20
申请号 RU20070137197 申请日期 2007.10.08
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "KONSTRUKTORSKOE BJURO "LUCH" 发明人 KIZIMOV ALEKSEJ TIMOFEEVICH;FROLOVA LJUDMILA EVGEN'EVNA;ALEKSEEV STANISLAV MIKHAJLOVICH;FROLOV VASILIJ FEDOROVICH
分类号 G01C23/00 主分类号 G01C23/00
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