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Simulation of Pilot Helicopter Control System Based on PID Control

摘要


Helicopter piloting has gradually become a way of transporting pilots in various ports. However the helicopter is a high-order, multi-variable, strongly coupled and unstable system that requires reliable and effective control methods for flight control. Based on the analysis of the 3-DOF helicopter system, a simplified system model of the 3-DOF helicopter is obtained.The PID controller is designed by using the conventional PID control method and a fast and effective simulation debugging GUI is designed to simulate the designed controller.The simulation results show that the simulation curves are stable at the expected values, which proves the controllability of the helicopter system and the effectiveness of PID control.

參考文獻


Li Yashuai, Shao Zongkai. Adaptive fuzzy H∞ mixed sensitivity robust control for three-degree-of-freedom helicopter system[J]. Sensors and Microsystems, 2018, 37(1): 74-78. DOI:10.13873/J.1000-978 7( 2018) 01-0074-05
Ahsene Boubakir,Salim Labiod,Fares Boudjema,et al. Designand experimentation of a self-tuning PID control applied to the 3DOF helicopter[J]. Archives of Control Sciences,2013,23(3): 311-331
Madhumita Pal,Franck Plestan,Abdelhamid Chriette. Discrete-time second-order-sliding-mode observer for state and unknown inputestimation: Application to a 3DOF helicopter[C]//2015 European Control Conference,Linz,Austria,2015:2914-2919
Sun Yujia, Yan Guoqing. Adaptive fuzzy PID attitude control for three-degree-of-freedom helicopters[J]. Electronic Design Engineering, 2017, 25(11): 73-76. DOI:10.14022/j.cnki.dzsjgc.2017.11.018
Zhou Wei, Wang Xiaodong. Three-degree-of-freedom helicopter control based on nonlinear output feedback[J]. Computer and Digital Engineering, 2017, 45(5): 917-922. DOI:10.3969/j.issn.1672-9722.201 7.05.027

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