Algorithm for Filtering Interference in the Navigation Flight Control System

Student: Turchaninova Marianna

Faculty: HSE Tikhonov Moscow Institute of Electronics and Mathematics (MIEM HSE)

Educational Programme: Infocommunication Technologies and Systems (Bachelor)

Year of Graduation: 2021

Attitude measurement systems, consisting of various devices, measure the angular velocity and acceleration in the navigation system, and are vulnerable to external interference. In this paper, we consider an algorithm for filtering noise in the flight navigation system using the selected filter model. All calculations are performed in the MATLAB numerical computing environment, which allows you to plot functions and data, implement algorithms, and create programs. The work consists of an overview of existing devices for the navigation system and filters, as well as calculations in the MATLAB environment. Expected Results - a program showing the operation of the filter on a specific example of an aircraft and graphs demonstrating the operation of the device with and without a filter.

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