Applied Mathematics & Information Sciences
Abstract
The modern flight control systems are complex since they have a non-linear nature. Also, modern aerospace vehicles are expected to have non-conventional flight envelopes and, in order to operate in uncertain environments, they must guarantee a high level of robustness and adaptability. A Neural Networks controller can be used in applications with manned or unmanned aerial vehicles. The paper shows the mathematical model for hexacopter dynamics and a comparison between two different technique for stabilization and trajectory control: proportional,integral, derivative controller and real rime system controller based on Neural Networks. Numerical simulations are performed in order to validate both mathematical model and control approaches.
Digital Object Identifier (DOI)
http://dx.doi.org/10.18576/amis/100202
Recommended Citation
Artale, Valeria; Collotta, Mario; Milazzo, Cristina; Pau, Giovanni; and Ricciardello, Angela
(2016)
"Real-Time System based on a Neural Network and PID Flight Control,"
Applied Mathematics & Information Sciences: Vol. 10:
Iss.
2, Article 2.
DOI: http://dx.doi.org/10.18576/amis/100202
Available at:
https://digitalcommons.aaru.edu.jo/amis/vol10/iss2/2