Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation

Autor:	V. V. Legkostup
Jazyk:	English<br />Russian
Rok vydání:	2021
Předmět:	curvilinear elliptic coordinate system lame coefficients navigation kinematics of navigation and guidance uav tdoa Information technology T58.5-58.64
Zdroj:	Sistemnyj Analiz i Prikladnaâ Informatika, Vol 0, Iss 3, Pp 15-24 (2021)
Druh dokumentu:	article
ISSN:	2309-4923 2414-0481
DOI:	10.21122/2309-4923-2021-3-15-24
Popis:	In this work, simplified expressions have been obtained that describe the kinematics parameters of the aircraft movement and its accelerations. These expressions are needed to obtain an optimal linear control law in order to provide movement of the aircraft using the hyperbola guidance method with a time difference of arrival navigation system. The key feature of the hyperbola navigation method is the ability to reduce the number of navigation positions by one when the on-board navigation equipment operates in a passive mode, carrying out only the reception of navigation information, like consumers of satellite navigation information.
Databáze:	Directory of Open Access Journals
Externí odkaz:	https://doaj.org/article/ecf0efc3c7874a2a9105c0179dafe104 Zobrazit plný text záznamu View record in DOAJ