Decoupling control for airspeed and flight path angle using an improved Total energy control algorithm

摘要：

An improved core algorithm is proposed for “Total Energy Control System(TECS), which diminishes the response oscillations caused by the cooperation error between aircraft total energy and its distribution. The construction of a feedback loop based on energy cooperation error to enhance decoupling performance for airspeed and flight path angle is the key step in the proposed approach. Based on the suggested method the TECS controller is synthesized for a linearized longitudinal axis aircraft model. Simulation results indicate that the cooperation error feedback loop can effectively reduce system response oscillations and achieves superior performance.

作者: Zhang Qingzhen Gao Chen Ma Wentao Ren Zhang

作者单位: School of Automation Science and Electronic Engineering Bei Hang University,Beijing,China

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 660-665

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）