Design of Thrust Regulation Law for Adjustable Lateral Thrust and Aerodynamics Blended Control Aerocraft

摘要：

　　The thrust regulation law for adjustable lateral thrust and aerodynamics blended control aerocraft is proposed in this paper.Firstly,lateral jet engine configuration and thrust characteristics are given,while the constraint conditions are analyzed.Secondly,the dynamic model of thrust regulating process is established,and the cost function and constraint conditions of the optimization problem are determined.In addition,the thrust regulation law is proposed based on dynamic system method.Then,the analytical form of the regulation law is presented by analyzing thrust regulation process of different quadrants.Finally,the feasibility of the thrust regulation law is verified by the simulation results.

关键词： adjustable lateral thrust regulation law cost function blended control

作者: ZHAO Yuyu YANG Baoqing

作者单位: Control and Simulation Center,Harbin Institute of Technology,Harbin 150001,China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 568-572

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）