deicing fluid

Robust Temperature Control Method for Aircraft Deicing Fluid with Observer

基于观测器的飞机除冰液温度鲁棒控制方法研究

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The Developing of Deicing Fluid Instant Heating System on Aircraft Deicing Vehicle

即热式飞机除冰车除冰液快速加热系统研制

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Deicing fluid heating control system design mainly includes outlet temperature control, temperature, pressure, flow display and alarm.

除冰液的加热控制系统设计主要内容包括出口温度的控制，温度、压力、流量的显示和报警等。

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The result of experiments and of the simulation show that the new type of aircraft deicing fluid instant heating system, with shorter preparing time and less energy cost, is satisfactory for its precise control and antijamming property.

试验与仿真结果表明，新型飞机除冰液快速加热系统较老式系统准备时间短，工作更节能，并有良好的精度及抗扰动性能。

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The aircraft deicing fluid temperature raising process model with time delay and parameter uncertainty was considered.

对飞机除冰液温升模型的时变和延时特性进行了分析研究。

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