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基于ADEMO/D-ENS的飞控系统性能指标分配方法
引用本文:刘志君,张新明,高亚奎,车军.基于ADEMO/D-ENS的飞控系统性能指标分配方法[J].测控技术,2019,38(7):109-112.
作者姓名:刘志君  张新明  高亚奎  车军
作者单位:航空工业北京青云航空仪表有限公司,北京,101399;航空工业第一飞机设计研究院飞控液压所,陕西西安,710089;航空工业自控所飞行控制一体化中电实验室,陕西西安,710065
基金项目:国家自然科学基金资助项目(61573286);航空科学基金项目(201505853043)
摘    要:针对目前飞行控制系统设计中部件/组件性能参数的确定存在反复多次迭代的问题,对飞控系统性能指标的分配进行了研究。通过对性能指标分配过程进行建模,确定了分配过程属于多目标优化问题。基于Tchebycheff方法将多目标优化问题转化为单目标优化子问题集合,基于自适应差分进化算法得到的单目标优化子问题集合的最优解即为多目标优化问题Pareto最优解,同时采用惩罚因子保持差分进化算法种群的多样性。通过仿真与性能指标未分配的系统进行对比,结果表明分配后的系统具有更好的动态性和跟踪性,说明所提出的分配方法是正确的、可行的,并能够为工程应用提供一定的理论指导。

关 键 词:飞行控制  指标分配  控制带宽  精度  优化  差分进化

Performance Indexes Allocation Method of Flight Control System Based on ADEMO/D-ENS
LIU Zhi-jun,ZHANG Xin-ming,GAO Ya-kui,CHE Jun.Performance Indexes Allocation Method of Flight Control System Based on ADEMO/D-ENS[J].Measurement & Control Technology,2019,38(7):109-112.
Authors:LIU Zhi-jun  ZHANG Xin-ming  GAO Ya-kui  CHE Jun
Affiliation:(AVIC Beijing Keeven Aviation Instrument Co.,Ltd.,Beijing 101399,China;Flight Control and Hydraulic System Design Institute,AVIC the First Aircraft Design Institute,Xi' an 710089,China;Science and Technology on Aireraft Control Laboratory,FACRI,Xi' an 710065,China)
Abstract:To solve the problem that the performance parameters of components/assemblies are repeatedly selected and replaced in the current flight control system design,the allocation of performance indexes of the flight control system is studied.By modeling the allocation process of the performance indexes,it was determined that the allocation process was a multi-objective optimization problem.The multi-objective optimization problem was transformed into a set of single-objective optimization sub-problems based on Tchebycheff method.The optimal solution of the set of single-objective optimization sub-problems based on adaptive differential evolution algorithm was the Pareto optimal solution of the multi-objective optimization problem.Meanwhile,penalty factors were used to maintain the diversities of the differential evolution algorithm population.Compared with the system with unallocated performance indexes,the results show that the allocated system has better dynamic and tracking performance,which illustrates the proposed allocation method is correct and feasible,and can provide certain theoretical guidance for practical application.
Keywords:flight control  indexes allocation  control bandwidth  precision  optimization  differential evolution
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