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INTEGRATED STRAPDOWN INERTIAL AND SATELLITE NAVIGATION SYSTEM ON COARSE SENSORS
INTEGRATED STRAPDOWN INERTIAL AND SATELLITE NAVIGATION SYSTEM ON COARSE SENSORS
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机译:粗传感器上集成的捷联惯导和卫星导航系统
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摘要
FIELD: engineering industry.;SUBSTANCE: strapdown inertial navigation system (SINS) includes three computing navigation platforms, each of which has its own control law. Each platform performs damping of inertial errors (IE) as per its own law. At that, inertial error depends on the main aircraft movement parametres: roll, heading derivative, horizontal constituent parts of linear carrier acceleration; also on data quality of source of satellite navigation system, which is external in relation to the system. Master filter receiving output platform signals performs their optimum processing.;EFFECT: improving accuracy.;5 cl, 7 dwg
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