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METHOD OF INCREASING ACCURACY OF INITIAL ALIGNMENT OF STRAPDOWN INERTIAL SYSTEM

机译:增加捷联惯性系统初始对准精度的方法

摘要

FIELD: information technology.;SUBSTANCE: invention, characterized as method of increasing accuracy of initial alignment of strap down inertial system (SDIS) during aircraft (AC) location at aerodrome, after initial alignment and transition SDIS in navigation mode, during AC location at aerodrome, combined processing of inertial calculation and external information, at least, from satellite navigation system (SNS), relates to inertial navigation and can be used in aircraft SDIS. Said information processing includes generating estimates of corrections to calibration values of primary errors SDIS and generating estimates of corrections to output parameters of inertial calculation. Combined processing of information further includes filtering obtained said estimates of corrections at conditions observability and reliability, wherein evaluation of corrections meets above criteria, and/or zero values for estimates, does not satisfy said criteria are introduced into the corresponding estimates of corrections to calibration values of primary errors SDIS and adjustments to estimates of inertial calculation output parameters, including orientation angles determined at stage of initial alignment, directly at moment of AC take-off from runway.;EFFECT: technical result is increase of accuracy of SDIS initial alignment.;3 cl
机译:领域:信息技术;发明:本发明的特征在于一种方法,其用于在机场的飞机(AC)定位,导航模式下的初始对准和过渡SDIS之后,机场,至少来自卫星导航系统(SNS)的惯性计算与外部信息的组合处理,与惯性导航有关,可用于飞机SDIS。所述信息处理包括生成对主误差SDIS的校准值的校正估计,以及生成对惯性计算的输出参数的校正估计。信息的组合处理还包括在条件可观察性和可靠性下过滤获得的所述校正估计,其中校正的评估满足上述标准,和/或将不满足所述标准的估计的零值引入到校准值的相应校正估计中SDIS的主要误差和惯性计算输出参数的估计值的调整,包括在初始对准阶段确定的定向角,直接在AC从跑道起飞时确定。 3厘升

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