摘要
建立了飞机座舱环境控制系统优化设计的数学模型，并对其优化设计方法进行了探讨．采用广义乘子法结合单纯形加速法，对目前军用机采用的４种环控系统进行了寻优。
The method for aircraft cabin environmental control system optimization has been approached,which includes establishment of mathematical model,determination of objective function and constraints,and selection of optimization technique.Four types of environmental control system presently used in military aircraft are considered.The general multiplier method combined with simplex method is applied to seek optimal one from these systems.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1996年第5期563-569,共7页
Journal of Beijing University of Aeronautics and Astronautics
关键词
座舱
环境控制
系统
最优设计
cabins
environmental control
systems
optimum design
