Control System Design of a Hex-Rotor Aircraft Based on the Neural Network Sliding Mode Method
2014 ◽
Vol 971-973
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pp. 418-421
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For the existing Multi-rotor aircrafts, the under-actuation and strong coupling characteristics have a remarkable influence on their flight performance. In order to overcome this effect, a novel Hex-Rotor aircraft is proposed in this paper. Based on the unique configuration of its six driving rotors, the Hex-Rotor aircraft has the ability to achieve the real independent control on the space 6-DOF channels. An autonomous flight control system with neural network sliding mode is designed. The simulation proved that the novel Hex-Rotor aircraft has desired maneuvering capability,and thehe control system is able to guarantee the aircrafts tracking flight of the aircraft.
2017 ◽
Vol 89
(6)
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pp. 764-776
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2021 ◽
pp. 095441002110455
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