基于飞行性能的多操纵面飞机控制分配方法  

Control allocation for aircraft with multiple control effectors based on flight performance optimization

作　　者：刘艳[1] 高正红[1] 

机构地区：[1]西北工业大学翼型叶栅空气动力学国防科技重点实验室,陕西西安710072

出　　处：《飞行力学》2010年第3期5-8,共4页Flight Dynamics

摘　　要：从飞行性能的角度,提出了多操纵面飞机空战阶段的控制分配原则及方法。以瑞典FOI开发的ADMIRE为算例,根据所提出的控制分配原则与方法对其控制分配器进行了重新设计。并比较了原飞机与采用新控制分配器飞机的空战周期时间,结果表明所建立的控制分配原则与算法是合理的。This paper discusses the control allocation principle and solution for aircraft with multiple control effectors from the angle of flight performance.The control selector of Aero-Data Model in Research Environment（ADMIRE） developed by FOI is redesigned based on the principle and solution developed in this paper as an example.The Combat Circle Time（CCT） of the original aircraft and ADMIRE with new control selector are compared with,the results indicate that ADMIRE with new control selector has a shorter CCT,which means the principle and solution developed in this paper are reasonable.

关 键 词：多操纵面 控制分配 飞行性能 控制分配器 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]