Development of a hybrid-fuzzy air temperature controller for a supersonic combustion test facility

被引：6

作者：

Owens, M ^{[1
]}

Segal, C ^{[1
]}

机构：

[1] Univ Florida, Gainesville, FL 32611 USA

来源：

EXPERIMENTS IN FLUIDS | 2001年 / 31卷 / 01期

关键词：

Hydrogen; Combustion; Fuzzy Logic; Setpoint; Control Method;

D O I：

10.1007/s003480000255

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

Hydrogen gas is burned in air to raise and maintain the stagnation temperature of a supersonic combustion test facility to a desired setpoint. In order to reach the desired operating conditions for stagnation temperature, there are three phases to the hydrogen control; Hz ignition at facility start-up, H-2 ramp-up while the facility is ramped-up, and H-2 iteration to achieve the desired temperature setpoint. Each phase incorporates a different type of control. Fuzzy logic is used to design a computer based supervisory controller that recognizes the different phases of operation and chooses the appropriate control method.

引用

页码：26 / 33

页数：8

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