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The DC converter control for deceleration profile in energy recovery from landing aircraft

机译:用于降落飞机能量回收的减速曲线的直流转换器控制

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This paper discuss about the Hcontrol strategy for DC converter in the energy recovery from landing aircraft. The energy from landing aircraft can be changed to electrical energy by using several power electronics converters combine with the linear generator. To have this effect the controllers must able to control the mechanical and electrical outputs. The mechanical outputs are such as the force, speed of the linear generator while the electrical outputs are the voltage and current. By using the H control strategy at the specific location especially at the converter side it hopes that all the outputs stated above can be controlled. The goals for this paper are to maintain the dc voltage value at the converter and to have constant deceleration speed and force at the linear generator in order to change the kinetic energy from landing aircraft to electrical energy. All the models and the simulations have been done in MATLAB software package.
机译:本文讨论了降落飞机能量回收中直流变换器的H 控制策略。通过将多个电力电子转换器与线性发电机结合使用,可以将来自飞机着陆的能量转换为电能。为了达到这种效果,控制器必须能够控制机械和电气输出。机械输出是例如线性发电机的力,速度,而电气输出是电压和电流。通过在特定位置(尤其是在转换器侧)使用H 控制策略,希望可以控制上述所有输出。本文的目标是保持转换器上的直流电压值,并在线性发电机上保持恒定的减速速度和作用力,以将飞机着陆时的动能转换为电能。所有模型和仿真均已在MATLAB软件包中完成。

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