Control System Design of a Hex-Rotor Aircraft Based on the Neural Network Sliding Mode Method

Abstract:

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.

• Periodical: Advanced Materials Research (Volumes 971-973)
• Pages: 418-421
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.971-973.418
• Online since: June 2014
• Authors: Chang Jun Zhao*, Yue Bai, Xun Gong, Dong Fu Xu, Zhi Jun Xu
• Keywords: Hex-Rotor Aircraft, Lagrangians, Neural Network (NN)

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