The Comparison of Conventional Yaw Axis control Versus Closed Loop Yaw Axis Control

摘要：

The primary flight control system (PFCS) provides full time and full authority three axis, dynamic control law functions (pitch, roll and yaw) and nondynamic control law functions (aileron droop, speed brake and ground lift dump). In addition, the PFCS calculates operational and limiting airspeed in order to provide full flight envelope protection across the entire flight envelope. PFCS provides limited gust alleviation function in the yaw axis. This paper provides a high level comparison of conventional Yaw Axis control (Pedal to Surface with Augmentation) versus Closed Loop Yaw Axis control. Pedal to Surface versus Closed Loop design options have implications on a variety of factors including Human Factors, Gust Response, structural limiting requirements, asymmetric thrust response, and rudder trim.

关键词： Conventional Yaw Axis Design Closed Loop Yaw Axis Design Gust Response Asymmetric thrust response Rudder Trim

作者: Ju Kunru Zhang Renjie XuDanli

作者单位: Information and Engineering Department of TV University Shanghai, China

会议类型: 国际会议

会议名称: 2011 IEEE 2nd International Conference on Computing，Control and Industrial Engineering(CCIE 2011)(第二届计算、控制与工业工程国际会议)

会议地点: 武汉

会议语种:英文

页码: 138-141

在线出版日期: 2011-08-20（万方平台首次上网日期，不代表论文的发表时间）