Reusable Launch Vehicle Lateral Control Design on Suborbital Reentry

摘要：

This paper presents the lateral/directional stability and control analysis and the control design results for the Reusable Launch Vehicle on suborbital reentry. The relative location of the open-loop quadratic poles and zeros is discussed. The feedback of roll rate to aileron is of better effectiveness to damping the Dutch roll than the feedback of yaw rate. To avoid the adverse yaw by ailerons, a yaw-to-roll concept method is developed using primarily rudder for lateral-directional control. The simulation shows that the rudder control roll method is practical.

作者: Liaoni Wu Yimin Huang ChengLong He

作者单位: College of Automation Engineering,Nanjing University of Aeronautics and Astronautic,Nanjing,210016,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: 885-889

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）