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Aerospace Instrument-Making

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REQUIREMENTS FOR UNMANNED AERIAL VEHICLES ON MULTI-ROTATIONAL BASIS
R.N. Nabiyev, A.T. Hazarkhanov, Q.I. Qarayev, A.A. Abdullayev, V.A. Abbasov

The article gives extended information on the requirements for the design and manufacture of a multi-rotor unmanned aerial vehicle (UAV), type as a hexacopter, with a modern automatic control system for civil and military use. In addition to this article: are given fl ight characteristics of the UAV; operating principle of the elements of the automated control system and their operation modes; the basic conditions for the design and manufacture of the hexacopter are determined, taking into account the low repair costs and the preparation time for the fl ight. Assignment of a UAV – hexacopter type: aerial photography and video shooting; meteorological monitoring of the environment; a flight with a relatively heavy payload, etc. To fulfi ll the above tasks, the article lists and selects the basic components of UAV elements, such as a hexacopter.
Keywords: unmanned aerial vehicle (UAV), hexakopter, automatic control system, navigation system, autonomous flight, barometer, Kalman filter, multi-rotation.


DOI: 10.25791/aviakosmos.09.2018.166

Contacts: E-mail: nabiyevrasim@gmail.com, E-mail: enver-xan@mail.ru, E-mail:qedir71@mail.ru, E-mail: anarcafarov09@mail.ru, E-mail: vusal9820@gmail.com

Pp. 03-11.

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