MULTI-FUNCTIONAL SINGLE-SEAT AIRCRAFT WITH INTEGRATED CONTROL SYSTEM

The invention relates to highly manoeuvrable aircraft with a multi-functional control system. The present aircraft comprises an integrated control system (ICS) which includes a computing unit connected by inputs and outputs to flight control surface actuators and propulsion unit swivelling nozzle ac...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KRYUCHKOV, Vladimir Vitalyevich, KONSTANTINOV, Sergey Valentinovich, ZAYEC, Viktor Fedorovich, KOSTENKO, Nikolay Ivanovich, ZALESSKIY, Sergey Yevgenyevich, SKACHKOV, Anatoliy Fedorovich, DYEMIN, Igor Mihailovich, KRASNOV, Vladimir Alekseevich, ZASOVIN, Aleksandr Igorevich, BELYAEV, Aleksey Valeryevich, MOSKALEV, Pavel Borisovich, KISLOV, Sergey Vladimirovich
Format:	Patent
Sprache:	eng ; fre ; rus
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONTROLLING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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