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UDC 681.5
DEVELOPMENT OF MEASUREMENT UAV ATTITUDE CONTROL UNIT WITH NON-ORTHOGONAL ARRANGEMENT OF SENSING ELEMENTS
Parshin Anatoly Pavlovich1, Nemshilov Yuri Alexandrovich2
1National Aerospace University of M. Ye. Zhukovsky "HAI", PhD, assistant professor of aircraft control systems
2National Aerospace University of M. Ye. Zhukovsky "HAI", PhD, assistant professor of aircraft control systems
1National Aerospace University of M. Ye. Zhukovsky "HAI", PhD, assistant professor of aircraft control systems
2National Aerospace University of M. Ye. Zhukovsky "HAI", PhD, assistant professor of aircraft control systems
Abstract
This article is devoted to solving problems RESILIENCE UAV attitude control systems by creating blocks of functional redundancy through the use of non-orthogonal arrangement of sensing elements. On the basis of the study authors suggest complexed measuring unit orientation system of MEMS inertial sensors.
Keywords: accelerometer, aggregation, an unmanned aerial vehicle, gyroscope, non-orthogonal arrangement, power system orientation, strapdown inertial navigation system
Article reference:
Development of measurement UAV attitude control unit with non-orthogonal arrangement of sensing elements // Modern technics and technologies. 2016. № 3 [Electronic journal]. URL: https://technology.snauka.ru/en/2016/03/9697
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