Differential Flatness Based Control of Glide-reentry Anti-vessel Missile Engineless Part

摘要：

Nonlinear inverse dynamic controller based on differential flatness was designed for Glide-reentry anti-vessel missile terminal engineless part.Aerodynamic data was processed to make the missile model flat.Brake rudder was introduced to control terminal energy and fulfill the requirement of flatness.

作者: LI Congying HAN Lei XU Xiaofei YU Jinyong

作者单位: 7th Department of Naval Aeronautical Engineering Institute ,Yantai 264001,P.R.China Ordnance Department of the Naval Equipment Division,Beijing 100841,P.R.China 3th Department of Naval Aeronautical Engineering Institute ,Yantai 264001,P.R.China

会议类型: 国际会议

会议名称: The 30th Chinese Control Conference(第三十届中国控制会议)

会议地点: 烟台

会议语种:英文

页码: 1-5

在线出版日期: 2011-07-01（万方平台首次上网日期，不代表论文的发表时间）