Multicopter flight control system

Аuthors

Kornilov V. A.^1*, Molodyakov D. S.^2**, Sinyavskaya Y. A.^***

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Experimental Design Bureau "Sukhoi", 23B, Polikarpov str., p/b 604, Moscow, 125284, Russia

*e-mail: valery.korn@mail.ru
**e-mail: molodyakov@inbox.ru
***e-mail: cijulia@mail.ru

Abstract

In the article we consider the problem ofsyntheses of multicopter flight control system, propose the variants of architecture of automatic control system. The basic flight modes and variants of control are described.

Keywords:

unmanned aerial vehicle; multicopter; automatic control; quasi-optimal control; Pontryagin maximum; Kalman-Buсy filter

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