Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival

This paper discusses the problem of determining a kinematics (in terms of transfer function, as far as possible) of parameters of the motion of an aircraft expressed in the curvilinear coordinate system and control accelerations expressed in a rectangular coordinate system. Examples of curvilinear c...

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Bibliographic Details
Main Authors: V. V. Legkostup, V. E. Markevich
Format: Article
Language:English
Published: Belarusian National Technical University 2021-04-01
Series:Sistemnyj Analiz i Prikladnaâ Informatika
Subjects:
uav
Online Access:https://sapi.bntu.by/jour/article/view/498