摘要： 针对在飞机除冰液加热系统中管路流量脉动造成温度波动的问题，提出单神经元PID控制策略，建立飞机除冰液加热系统的数学模型，并使用Matlab进行仿真。结果表明，单神经元PID控制策略对飞机除冰液加热过程的控制，比常规的PID控制器速率快、稳定 性高。

关键词: 除冰液, 加热系统, 单神经元, PID控制, 扰动抑制

Abstract: Aiming at the temperature turbulence problem of aircraft deicing heating system, this paper presents the single neuron PID control strategy which combines the advantage of conventional PID control with artificial neuron control. By building the mathematical model of aircraft deicing fluids heating system on the basis of data gathered by experiments, simulation of single neuron PID control is executed. Results show that the single neuron PID control strategy performs effectively on the temperature turbulence problem of aircraft deicing fluids heating system.

Key words: deicing fluids, heating system, single neuron, PID control, turbulence resistance

中图分类号: 

• TP391