Model of dynamic descriptions of the strapdown inertial system
DOI:
https://doi.org/10.18372/2073-4751.2.6788Abstract
The ways of decrease in expenses for certified tests are analyzed. The mathematical model of inertial navigation system is offered
References
Руководство по требуемым навига-ционным характеристикам, DOC9613AN1937, ICAO, 1999.
Единые западноевропейские нормы летной годности. Всепогодные полеты, JAR-AWO, 1996.
Казак В.Н., Салимон В.И., Туник А.А. Системы автоматического и полуавтоматического управления полетом. – К.: НАУ, 2001. – 201 с.
Методика оценки соответствия точности характеристик систем автоматического управления эксплуатационным требованиям вероятности недопустимых ошибок управления. Летноисследовательский институт им. М.М. Громова, 1993.
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