COMPARATIVE ANALYSIS OF INFORMATION INTEGRATION SCHEMES STERILE INERTIAL NAVIGATION SYSTEMS FOR UNMANNED VEHICLES AIRCRAFT

Authors

  • P. Ermakov Государственный научно-исследовательский институт авиационных систем, ГосНИИАС
  • A. Gogolev Ермаков П.Г.*, Гоголев А.А.** Государственный научно-исследовательский институт авиационных систем, ГосНИИАС

DOI:

https://doi.org/10.31618/ESSA.2782-1994.2021.3.76.213

Keywords:

имитационное моделирование; беспилотный летательный аппарат; навигационная система; раздельная схема комплексирования; слабосвязанная схема комплексирования; фильтр Калмана

Abstract

A serious problem with modern unmanned aerial vehicles weighing less than 500 kg is their low reliability due to the significant mass limitations of the information management complex, which in turn leads to the use of microelectromechanical (MEMA) Sensors with significant care and drift [1]. This article provides a comparative analysis of the separate and loosely linked integration schemes based on the simulation of the VN-100T inertial-measurement module and navigation algorithms with the aim of increasing the accuracy and reliability of the informationThe manager of the unmanned aerial vehicle (UAV) complex.

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Published

2022-01-27

Issue

Vol. 3 No. 12(76) (2021)

Section

Статьи

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