摘要
建立了主动控制起落架的非线性振动模型，并通过建立系统的状态方程和合理的目标函数，使系统的综合性能达到最优。通过数值模拟计算，对主动控制起落架和被动起落架的滑行性能进行了比较。
A non linear model of active control of the landing gear has been established. According to the state equations and a reasonable objective function, the comprehensive performance of landing gear is optimized. By numerical simulation, the taxiing performance of an active control system landing gear and that of a passive system landing gear are compared.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1999年第6期545-548,共4页
Acta Aeronautica et Astronautica Sinica
关键词
起落架
主动控制
非线性振动
滑行性能
飞机
landing gear
active control
non linear vibration
taxiing performance
