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Salvatore Rosario Bassolillo, Luciano Blasi, Egidio D?Amato, Massimiliano Mattei and Immacolata Notaro
This paper deals with the design of a guidance control system for a swarm of unmanned aerial systems flying at a given altitude, addressing flight formation requirements that can be formulated constraining the swarm to be on the nodes of a triangular mes...
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Majed Swaid, Tobias Marks, Florian Linke and Volker Gollnick
The operational concept of aerodynamic formation flight, also referred to as aircraft wake-surfing for efficiency (AWSE), has high potential in terms of fuel savings and climate impact mitigation. In order to implement this concept, many technological an...
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Jose I. Rojas, Marc Melgosa and Xavier Prats
Wake vortex encounters (WVE) can pose significant hazard for en-route aircraft. We studied the sensitivity of wake vortex (WV) circulation and decay to aircraft mass, altitude, velocity, density, time of catastrophic wake demise event, eddy dissipation r...
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Mohammadreza Amoozgar, Michael I. Friswell, Seyed Ahmad Fazelzadeh, Hamed Haddad Khodaparast, Abbas Mazidi and Jonathan E. Cooper
In this paper, the effect of distributed electric propulsion on the aeroelastic stability of an electric aircraft wing was investigated. All the electric propulsors, which are of different properties, are attached to the wing of the aircraft in different...
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Petr Kazarin, Anton Provalov, Vladimir Golubev, Sherry Borener, ... Alex Suchkov
Pág. 1364 - 1373
The paper presents results of the vortex safety analysis conducted for selected unmanned aircraft systems (UAS) operating alongside commercial aircraft in the terminal zone. The approach is developed on the basis of a dynamic model of an aircraft enterin...
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