54040

Автор(ы): 

Автор(ов): 

9

Параметры публикации

Тип публикации: 

Статья в журнале/сборнике

Название: 

Enhancement of INS/GNSS integration capabilities for aviation-related applications

ISBN/ISSN: 

20751087

DOI: 

10.1134/S2075108717040101

Наименование источника: 

  • Gyroscopy and Navigation

Обозначение и номер тома: 

Vol. 8, iss. 4

Город: 

  • New York, NY, USA

Издательство: 

  • Pleiades Publishing, Ltd.

Год издания: 

2017

Страницы: 

248-258
Аннотация
Two methods for construction and use of integrated inertial and satellite systems are considered, taking into account the specific features of aviation-related applications, namely, alignment correction, and autocalibration. Alignment correction is performed during aircraft maneuvering on the airfield. Autocalibration of strapdown inertial navigation systems (SINS) is based on using the estimations of instrumental errors of inertial sensors, which had been obtained by the complex information processing (CIP) algorithm in a number of previous flights of the aircraft. The results of numerous flight tests of laser SINS designed by PAO MIEA for civil and military applications are provided as an evidence of high efficiency of the information integration methods proposed herein.

Библиографическая ссылка: 

Зорина О.А., Измайлова Е.А., Кухтевич С.Е., Портнов Б.И., Фомичёв А.В., Вавилова Н.Б., Голован А.А., Папуша И.А., Парусников Н.А. Enhancement of INS/GNSS integration capabilities for aviation-related applications // Gyroscopy and Navigation. 2017. Vol. 8, iss. 4. С. 248-258.

Публикация имеет версию на другом языке: 

Да

Связь с публикацией: