A new application of the hardware in the loop test of the min–max controller for turbofan engine fuel control

M. Davoodi, H. Bevrani
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Abstract

This article performs a novel hardware test application on the min–max algorithm to control a two-axis turbofan engine's fuel with a high bypass ratio. In this technique the microcontroller uses a nonlinear model based on the min–max algorithm to control the turbofan's fuel consumption. The min–max control method precisely provides the desired thrust while meeting the engine's physical and operational limitations. By setting the engine's limits appropriately, a surge is prevented from happening due to overheating of the turbine. As a proof of concept, the proposed fuel control algorithm is verified using an Intel Addison's Arduino microcontroller connected to a computer. The implemented hardware is examined by incorporating it into a typical control loop test and monitored via a computer. The achieved results indicate fast time response and algorithm flexibility in simulation modes. The test results confirm the precision and proper implementation of the proposed min–max control algorithm. In addition, the suggested min–max control algorithm can be applied to realize restrictions such as the rotational speed and the outlet pressure of the high-pressure compressor under the required conditions.

Abstract Image

涡扇发动机燃油控制最小-最大控制器硬件在环测试的新应用
本文对高涵道比双轴涡扇发动机燃油控制的最小-最大算法进行了一种新颖的硬件测试应用。在该技术中,微控制器使用基于最小-最大算法的非线性模型来控制涡扇发动机的燃料消耗。最小-最大控制方法精确地提供所需的推力,同时满足发动机的物理和操作限制。通过适当设置发动机的极限,可以防止由于涡轮过热而发生喘振。作为概念验证,使用连接到计算机的Intel Addison’s Arduino微控制器验证了所提出的燃料控制算法。所实现的硬件通过将其结合到典型的控制回路测试中进行检查,并通过计算机进行监控。所获得的结果表明,在模拟模式下,快速的时间响应和算法的灵活性。测试结果证实了所提出的最小-最大控制算法的准确性和正确实现。此外,建议的最小-最大控制算法可用于在所需条件下实现高压压缩机的转速和出口压力等限制。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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CiteScore
2.60
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