Title :
A learning based approach for reduction of the pendulum behavior of ducted-fan helicopter
Author :
Yin Wang ; Daobo Wang ; Hongqiang Wang
Author_Institution :
Coll. of Astronaut., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Abstract :
Pendulum-like behavior of the helicopter is an effect occurs in the case where the movement of the body of the helicopter lags with respect to its rotors, leading to undesired oscillations when the helicopter is required to hover at desired positions. In this paper, an online learning based controller is designed to dampen the oscillation by coupling a two layers forward neural network with a classical PD control method. The neural network is able to approximate the nonlinear dynamics of the pendulum in an online manner, thus improving the overall performance of the linear PD controller. Simulations results have shown that the proposed technique is capable of suppressing the undesired oscillation in an automated manner and alleviating the needs for adjusting the tuning parameters of the controller.
Keywords :
PD control; control system synthesis; helicopters; learning systems; linear systems; neurocontrollers; nonlinear dynamical systems; oscillations; classical PD control method; ducted-fan helicopter; learning based approach; linear PD controller; nonlinear dynamics; online learning based controller; pendulum behavior reduction; tuning parameters; two layers forward neural network; undesired oscillations; Aerospace control; Biological neural networks; Conferences; Helicopters; Oscillators; PD control; Rotors;
Conference_Titel :
Control & Automation (ICCA), 11th IEEE International Conference on
Conference_Location :
Taichung
DOI :
10.1109/ICCA.2014.6870976