Development of a hybrid-fuzzy air temperature controller for a supersonic combustion test facility |
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Authors: | M. Owens C. Segal |
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Affiliation: | (1) PO Box 116250, University of Florida Gainesville, FL 32611, USA e-mail: cor@aero.ufl.edu Tel.: +1-352-3926132, US |
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Abstract: | 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; H2 ignition at facility start-up, H2 ramp-up while the facility is ramped-up, and H2 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. Received: 28 November 1999/Accepted: 2 November 2000 |
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