Abstract
Tiltrotor aircraft combines the vertical takeoff and Landing (VTOL) capability of helicopters with the high speed performance of turboprop airplanes. A longitudinal rigid body tiltrotor model is developed in this paper. Because it is very difficult to obtain the accuracy model, this paper investigates the theory about the fuzzy logic control and genetic algorithm. Then this theory is used to design the tiltrotor aircraft flight controller. Numerical methods are investigated and numerical simulation is conducted to account for the good flight controller designed based on Fuzzy Logic control via GA of the tiltrotor aircraft.
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© 2013 Springer-Verlag Berlin Heidelberg
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Chen, H., Wang, X., Lei, T. (2013). TiltRotor Aircraft Flight Control Study Based on Fuzzy Logic Control via Genetic Algorithm. In: Sun, Z., Deng, Z. (eds) Proceedings of 2013 Chinese Intelligent Automation Conference. Lecture Notes in Electrical Engineering, vol 254. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38524-7_41
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DOI: https://doi.org/10.1007/978-3-642-38524-7_41
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Online ISBN: 978-3-642-38524-7
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