摘要
针对倾斜转弯导弹的具体特点, 提出了一种基于模型参考时变全程滑态变结构控制理论的协调式耦合自动驾驶仪的设计方法, 并分别针对滚转通道、俯仰/偏航耦合通道进行了设计分析; 最后进行了三通道联合仿真,
Based on the time-varying sliding-mode variable structure adaptive control theories, a new coordinate coupling autopilot design scheme for BTT missiles is proposed. Design for roll channel and pitch/yaw coupling channel is also analised respectivly. Finally, the outstanding feature of our design is proved by digital simulations results.
出处
《航天控制》
CSCD
北大核心
1999年第4期22-26,共5页
Aerospace Control
关键词
倾斜转弯技术
变结构控制
自动驾驶仪
导弹
Bank-to-turn technique
Variable structure
Control Automatic pilot
Missile
