Упрощение модели ошибок инерциальной навигации при различных видах движения летательного аппарата

Abstract

To research observability of tool errors of sensitive elements strapdown inertial navigating system without simplification of initial model of errors of strapdown inertial navigating system it is practically impossible. At the same time there is an assumption, that at the certain maneuvers of the air flying device, corresponding errors of sensitive elements can be neglected and therefore will be possible to receive much more simple models of errors of strapdown inertial navigating system. Therefore represents practical interest to receive the simplified models of errors of strapdown inertial navigating system suitable for the subsequent analysis tool errors of sensitive elements observability