首页> 外文会议>Asia Simulation Conference/International Conference on System Simulation and Scientific Computing vol.1; 20051024-27; Beijing(CN) >A Novel Type of Nonlinear PID Controller with FFC for 3-DOF High Performance Flight Simulation Servo System
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A Novel Type of Nonlinear PID Controller with FFC for 3-DOF High Performance Flight Simulation Servo System

机译:三自由度高性能飞行仿真伺服系统的新型带FFC的非线性PID控制器

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摘要

This paper proposes a novel type of nonlinear PID(Proportional-Integral- Derivative) with FFC(feedforward controller) control strategy for 3-DOF(three degree of freedom) high performance flight simulation servo system. Firstly, the body structure of the 3-DOF high performance flight simulation servo system is described. Then, on the basis of detailed introduction of nonlinear PID theory, a novel nonlinear PID controller with additional FFC is developed. Three close-loop control architecture is adopted in the whole flight simulation servo system, and the idea of modularization design is adopted in the IPC(industrial personal computer) software. The hardware-in-the-loop simulation results, which based on a type of helicopter dynamic model, demonstrate that the flight simulation servo system using the proposed control scheme could achieve high performance in motion tracking and has strong robustness.
机译:针对三自由度(3自由度)高性能飞行仿真伺服系统,提出了一种新型的带有FFC(前馈控制器)控制策略的非线性PID(比例积分微分)算法。首先,描述了三自由度高性能飞行模拟伺服系统的主体结构。然后,在详细介绍非线性PID理论的基础上,开发了一种带有附加FFC的新型非线性PID控制器。整个飞行模拟伺服系统采用了三种闭环控制架构,而工业个人计算机(IPC)软件则采用了模块化设计的思想。基于一种直升机动力学模型的半实物仿真结果表明,采用所提出的控制方案的飞行仿真伺服系统可以实现高性能的运动跟踪,并且具有很强的鲁棒性。

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