MATHEMATICAL MODEL OF SELF-REPAIRING FLIGHT CONTROL  

自修复飞行控制的数学模型(英文)

作　　者：王永[1] 詹训慧[1] 吴刚[1] 胡寿松[2] 

机构地区：[1]中国科学技术大学自动化系 [2]南京航空航天大学自动化学院

出　　处：《Transactions of Nanjing University of Aeronautics and Astronautics》2003年第2期178-183,共6页南京航空航天大学学报（英文版）

摘　　要：The most prospective method for certain structural failures and damages that cannot employ redundancy is self-repairing techniques, to ensure especially the maximum flight safety. Based on the characters of self-repairing aircraft, this paper states some basic assumptions of the self-repairing aircraft, and puts forward some special new conceptions concerning the self-repairing aircraft: control input, operating input, command input, repair input and operating and control factor as well as their relationships. Thus it provides a simple and reliable mathematical model structure for the research on the self-repairing control of the aircraft.对于无法使用冗余技术的结构故障及损伤 ,欲最大可能地保证飞机的飞行安全 ,最有前景的方法是采用自修复技术。本文根据自修复飞机的特点 ,明确规范了自修复飞机的若干基本假设 ,提出了自修复飞机控制输入、操纵输入、指令输入、修复输入以及操控因子等特有的新概念 ,以及它们之间的相互关系 。

关 键 词：SELF-REPAIRING flight control mathematical model operating and control factor 

分 类 号：V249.12[航空宇航科学与技术—飞行器设计]