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A novel type of nonlinear PID controller with FFC for 3-DOF high performance flight simulation servo system

  • Haibin Duan*
  • , Daobo Wang
  • , Xiufen Yu
  • *此作品的通讯作者
  • Nanjing University of Aeronautics and Astronautics
  • CAS - National Space Science Center

科研成果: 会议稿件论文同行评审

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.

源语言英语
795-799
页数5
出版状态已出版 - 2005
活动Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005 - Beijing, 中国
期限: 24 10月 200527 10月 2005

会议

会议Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005
国家/地区中国
Beijing
时期24/10/0527/10/05

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