直升机悬架抗摆控制硬件在环仿真平台研究

Zhifu Tang, D. Yuan, Junfei Zhang, Xiaojun Xing, Cai Xin, Yuquan He
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引用次数: 1

摘要

为解决真实直升机抗摆控制试验准备周期长、成本高、风险大的问题,设计了直升机吊挂系统抗摆控制硬件在环仿真平台。采用六自由度机器人模拟直升机吊挂载荷的运动,通过带机械臂的外控导轨模拟吊挂载荷在机身纵向上的大摆动。本文设计了抗摆控制器,实现了直升机吊挂载荷的抗摆控制,同时进行了硬件在环仿真实验。实验结果表明,悬挂载荷在横向和纵向上相对于机身的摆角/角速度逐渐收敛并趋近于零,同时机器人的振动幅值越来越小。验证了该硬件在环仿真平台可用于直升机悬架抗摆控制研究。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on Hardware-in-loop Simulation Platform of Anti-swing Control for Helicopter Suspension
In order to solve the problems of long preparation period, high cost and high risk in anti-swing control test for real helicopter, a hardware-in-loop(HIL) simulation platform of anti-swing control for helicopter slung load system is designed. 6-DOF robot is employed to imitate the movement of the slung load for helicopter, and the large swing of the slung load in the longitudinal direction the fuselage is simulated by external control rail with robot arm. In this paper, the anti-swing controller is designed to realize the anti-swing control of the helicopter slung-load, at the same time, hardware-in-loop simulation experiment is carried out. The experimental results show that the swing angle/angular velocity of the slung load which relative to the fuselage in the lateral and longitudinal directions can converge and close to zero gradually, meanwhile the vibration amplitude of the robot becomes more and more smaller. So it proves that the hardware-in-loop simulation platform can be used to study anti-swing control for helicopter suspension.
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