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高压除水环境控制系统的解耦控制
引用本文:何君,赵竞全,袁修干.高压除水环境控制系统的解耦控制[J].北京航空航天大学学报,2002,28(2):225-227.
作者姓名:何君  赵竞全  袁修干
作者单位:北京航空航天大学,飞行器设计与应用力学系,北京,100083
摘    要:高压除水环境控制系统是典型的多输入多输出(MIMO)复杂控制系统,各个变量之间存在很强的耦合关系.试飞证明,采用传统的PID控制方法不能很好的解决电子设备和座舱的冷却问题,最明显的就是电子设备舱的冷却效果不佳.因此,对现有的飞机环境控制系统(ECS)必须加以改进.通过仿真表明,采用输出反馈、静态解耦控制后的环境控制系统能够满足系统设计要求.

关 键 词:飞机系统  环境控制  解耦
文章编号:1001-5965(2002)02-0225-03
收稿时间:2000-09-15
修稿时间:2000年9月15日

Decoupling Control of Aircraft Environmental Control System with High Pressure Water Separation
HE Jun,ZHAO Jing-quan,YUAN Xiu-gan.Decoupling Control of Aircraft Environmental Control System with High Pressure Water Separation[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(2):225-227.
Authors:HE Jun  ZHAO Jing-quan  YUAN Xiu-gan
Institution:Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics
Abstract:Aircraft environmental control system(ECS) with high pressure water separation is a representative complex coupling control system of MIMO. Flight tests proved that the controlling means with conventional PID control could not refrigerate the electronic equipment and the cabin satisfactorily. An attempt was made to use the controlling means of output feedback and static decoupling to improve the actual aircraft ECS. Through computer simulation, it was demonstrated that the improved aircraft ECS can satisfy the system design demands.
Keywords:aircraft systems  environmental control  decoupling  
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