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 。
