先进战斗机控制分配方法研究综述  

Development of Advanced Fighter Control Allocation methods

作　　者：王美仙[1] 李明[1] 

机构地区：[1]沈阳飞机设计研究所,辽宁沈阳110035

出　　处：《飞机设计》2006年第3期17-19,共3页Aircraft Design

摘　　要：综述了先进战斗机控制分配方法的研究和应用状况。文中首先介绍了4种主要的控制分配方法———广义逆法、串接链法、直接分配法和数学规划法,给出各种方法在飞行控制系统分配应用中的限制,然后简单介绍控制分配方法在现实飞行控制系统中的应用情况,最后对控制分配中的几个关键问题进行了分析总结。Research and application of advanced fighter control allocation methods were surveyed in this article. Firstly, four most important methods that are the generalized inverse, daisy chaining, direct allocation and mathematic programming are presented and limitations in application of these methods to flight control systems are discussed. Secondly, application of these allocation methods to several technology demonstrator programs is presented. Finally, several key problems on control allocation are analyzed and summarized.

关 键 词：多操纵面 控制分配 飞行控制系统 

分 类 号：V249.122[航空宇航科学与技术—飞行器设计]