Velocity Control of Unmanned Helicopter Based on Fuzzy-PID

Author:

Chen Xian Xiang1,Liu Ying1,Hu Xiong Wen1,Qian Yi1,Wang Jin Hua2

Affiliation:

1. Beijing Institute of Computer Application

2. China Academy of Ordnance Science

Abstract

The fuzzy-PID control approach was used on the velocity control of the unmanned helicopter. Furthermore, a novel parameter self-tuning method was presented that the parameters of the PID controller were self-tuned based on the parameters of the last control period according to the deviation and its variation ratio, adequately considering the control information of the last control period. The increments of the PID parameters were calculated by the fuzzy inference system. Matlab simulation and the hardware-in-loop simulation were performed, the simulation results verified the feasibility and the effectiveness.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Reference5 articles.

1. Le Zhang, Shaojie Bi, Hong Yang. Fuzzy-PID Control Algorithm of the Helicopter Model Flight Attitude Control, Control and Decision Conference (CCDC), 2010, Chinese, 1438 – 1443.

2. Dai Meihong. Attitude control of helicopter model based on fuzzy PID control[D]. Northeastern university, (2005).

3. Ji Jian, Jiang Ju. A model helicopter self-retun system based on fuzzy PID control[J]. Aircraft design, 2011, 31(1): 61-66.

4. Zhang Defeng. MATLAB fuzzy system design, national defense industry press, (2009).

5. Fuzzy Logic Toolbox User's Guide, Mathworks, (2010).

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