摘要
本文应用多变量不确定性系统的模型参考变结构自适应控制理论设计了某型BTT导弹协调式耦合变结构自动驾驶仪,有效地克服了通道间的交叉耦合效应,较好地保证了BTT导弹偏航通道与滚动通道之间的协调动作。
The Bank to Turn (BTT) missile coordinated couple variable structure autopilot,which is designed by model reference variable structure adaptive control theory for multivariable uncertain system,efficiently overcomes the cross coupled influence among three channels,guarantees the coordination between BTT missile's yaw channel and roll channel,and obtains the satisfactory instruction following performance
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1997年第1期8-12,共5页
Journal of Astronautics
关键词
BTT
导弹
自动驾驶仪
变结构
BTT missile Autopilot Variable Structure Model Reference