摘要
进行了自修复飞行控制系统各操纵面的单独／组合故障分类；研究了不同种类、不同组合、不同程度的故障下的飞机特性，分析了各种故障的影响；针对不同的故障模式分别进行了控制律重构设计并对飞机重构后的稳定性及操纵品质进行了仿真研究。结果表明，在非极端故障下，现有操纵面权限范围内，可以保证稳定飞行并具有可接受的操纵品质。
In this paper,control surface single or combination failures of an aircraft for selfrepairing flight control system are classified,the response of the aircraft under various type,various combination and different extent failures are studied. The reconfigurable control laws for different failures are designed and the simulation results show that the stable flight and satisfied handling qualities can be obtained except the extreme serious failures.
出处
《飞行力学》
CSCD
北大核心
1997年第3期67-72,共6页
Flight Dynamics
关键词
自修复
飞行控制系统
操纵面
补偿重构
Selfrepairing flight control system Failure model Reconfigurable design
