roll autopilot

A composite sliding mode control method for the design of missile roll autopilot is proposed.

针对导弹滚转驾驶仪模型,提出了一种复合滑模控制方案.

The Research on Design Method of Vehicle Roll Autopilot

飞行器滚动自动驾驶仪设计方法研究

When the autopilot is disengaged, the control wheels and ailerons move to the ( possibly undesired) neutral point and the airplane will roll proportional to the amount of trim input.

一旦自动驾驶被脱开，操纵盘和副翼就移向新的（可能是不需要的）中立点，并且，飞机将与配平输入量成比例地滚转。

A model tracing variable structure control methodology based on nonsingular terminal mode for second-order uncertain systems is proposed. Using this method, BTT roll channel autopilot is designed.

进一步提出基于非奇异终端滑模的二阶不确定系统的模型跟踪变结构控制方案，并将其应用于BTT导弹滚转通道的自动驾驶仪设计。

Sliding mode control method for the design of roll autopilot was proposed.

提出了一种滑模变结构滚转驾驶仪的设计方法.